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Updated cost in postings function
This commit is contained in:
Arthur Idema
parent
8335fd70d7
commit
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batch_search_eval.sh
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batch_search_eval.sh
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#!/bin/bash
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# Batch search and evaluation for Zoekeend results
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# Usage: ./batch_search_eval.sh <results_dir>
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if [ "$#" -ne 1 ]; then
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echo "Usage: $0 <results_dir>"
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exit 1
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fi
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RESULTS_DIR="$1"
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QUERIES_FILE="cranfield_queries.tsv"
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QRELS_FILE="cranfield_qrels.tsv"
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ZOEKEEND_PATH="./zoekeend"
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find "$RESULTS_DIR" -name "*.db" | while read DB_FILE; do
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BASE=$(basename "$DB_FILE" .db)
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RESULTS_FILE="$RESULTS_DIR/${BASE}_results.txt"
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EVAL_FILE="$RESULTS_DIR/${BASE}_eval.txt"
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echo "Running search for $DB_FILE..."
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"$ZOEKEEND_PATH" search "$DB_FILE" "$QUERIES_FILE" -o "$RESULTS_FILE"
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echo "Running evaluation for $RESULTS_FILE..."
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"$ZOEKEEND_PATH" eval "$RESULTS_FILE" "$QRELS_FILE" > "$EVAL_FILE"
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done
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echo "All searches and evaluations completed."
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1837
cranfield_qrels.tsv
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1837
cranfield_qrels.tsv
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File diff suppressed because it is too large
Load Diff
225
cranfield_queries.tsv
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225
cranfield_queries.tsv
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1 what similarity laws must be obeyed when constructing aeroelastic models of heated high speed aircraft .
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2 what are the structural and aeroelastic problems associated with flight of high speed aircraft .
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3 what problems of heat conduction in composite slabs have been solved so far .
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4 can a criterion be developed to show empirically the validity of flow solutions for chemically reacting gas mixtures based on the simplifying assumption of instantaneous local chemical equilibrium .
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5 what chemical kinetic system is applicable to hypersonic aerodynamic problems .
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6 what theoretical and experimental guides do we have as to turbulent couette flow behaviour .
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7 is it possible to relate the available pressure distributions for an ogive forebody at zero angle of attack to the lower surface pressures of an equivalent ogive forebody at angle of attack .
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8 what methods -dash exact or approximate -dash are presently available for predicting body pressures at angle of attack.
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9 papers on internal /slip flow/ heat transfer studies .
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10 are real-gas transport properties for air available over a wide range of enthalpies and densities .
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11 is it possible to find an analytical, similar solution of the strong blast wave problem in the newtonian approximation .
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12 how can the aerodynamic performance of channel flow ground effect machines be calculated .
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13 what is the basic mechanism of the transonic aileron buzz .
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14 papers on shock-sound wave interaction .
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15 material properties of photoelastic materials .
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16 can the transverse potential flow about a body of revolution be calculated efficiently by an electronic computer .
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17 can the three-dimensional problem of a transverse potential flow about a body of revolution be reduced to a two-dimensional problem .
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18 are experimental pressure distributions on bodies of revolution at angle of attack available .
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19 does there exist a good basic treatment of the dynamics of re-entry combining consideration of realistic effects with relative simplicity of results .
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20 has anyone formally determined the influence of joule heating, produced by the induced current, in magnetohydrodynamic free convection flows under general conditions .
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21 why does the compressibility transformation fail to correlate the high speed data for helium and air .
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22 did anyone else discover that the turbulent skin friction is not over sensitive to the nature of the variation of the viscosity with temperature .
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23 what progress has been made in research on unsteady aerodynamics .
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24 what are the factors which influence the time required to invert large structural matrices .
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25 does a practical flow follow the theoretical concepts for the interaction between adjacent blade rows of a supersonic cascade .
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26 what is a single approximate formula for the displacement thickness of a laminar boundary layer in compressible flow on a flat plate .
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27 how is the design of ring or part ring wings by linear theory affected by thickness .
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28 what application has the linear theory design of curved wings .
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29 what is the effect of cross sectional shape on the flow over simple delta wings with sharp leading edges .
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30 papers on flow visualization on slender conical wings .
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31 what size of end plate can be safely used to simulate two-dimensional flow conditions over a bluff cylindrical body of finite aspect ratio .
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32 to find an approximate correction for thickness in slender thin-wing theory .
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33 how do interference-free longitudinal stability measurements (made using free-flight models) compare with similar measurements made in a low-blockage wind tunnel .
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34 have wind tunnel interference effects been investigated on a systematic basis .
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35 are there any papers dealing with acoustic wave propagation in reacting gases .
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36 has anyone investigated relaxation effects on gaseous heat transfer to a suddenly heated wall .
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37 are there any theoretical methods for predicting base pressure .
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38 does transition in the hypersonic wake depend on body geometry and size
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39 how can one detect transition phenomena in boundary layers .
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40 how can one detect transition phenomena in hypersonic wakes .
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41 has anyone investigated and developed a simple model for the vortex wake behind a cruciform wing .
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42 what is a criterion that the transonic flow around an airfoil with a round leading edge be validly analyzed by the linearized transonic flow theory .
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43 can the transonic flow around an arbitrary smooth thin airfoil be analysed in a simple approximate way .
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44 what are the details of the rigorous kinetic theory of gases . (chapman-enskog theory) .
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45 has anyone investigated the effect of surface mass transfer on hypersonic viscous interactions .
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46 what is the combined effect of surface heat and mass transfer on hypersonic flow .
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47 what are the existing solutions for hypersonic viscous interactions over an insulated flat plate .
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48 what controls leading-edge attachment at transonic speeds .
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49 can the three-point boundary-value problem for the blasius equation be integrated numerically, using suitable transformations, without iteration on the boundary conditions .
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50 what are the effects of small amounts of gas rarefaction on the characteristics of the boundary layers on slender bodies of revolution .
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51 what is the available information pertaining to boundary layers on very slender bodies of revolution in continuum flow (the ?transverse curvature effect) .
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52 what is the available information pertaining to the effect of slight rarefaction on boundary layer flows (the ?slip? effect) .
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53 what investigations have been made of the flow field about a body moving through a rarefied, partially ionized gas in the presence of a magnetic field .
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54 how is the heat transfer downstream of the mass transfer region effected by mass transfer at the nose of a blunted cone .
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55 to what extent can the available information for incompressible boundary layers be applied to problems involving compressible boundary layers .
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56 to what extent can readily available steady-state aerodynamic data be utilized to predict lifting-surface flutter characteristics .
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57 what are the significant steady and non-steady flow characteristics which affect the flutter mechanism .
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58 is it possible to determine rates of forced convective heat transfer from heated cylinders of non-circular cross-section, (the fluid flow being along the generators) .
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59 how much is known about boundary layer flows along non-circular cylinders .
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60 is there any simple, but practical, method for numerical integration of the mixing problem (i.e. the blasius problem with three-point boundary conditions) .
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61 does there exist a closed-form expression for the local heat transfer around a yawed cylinder .
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62 how far around a cylinder and under what conditions of flow, if any, is the velocity just outside of the boundary layer a linear function of the distance around the cylinder .
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63 where can i find pressure data on surfaces of swept cylinders .
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64 can't the static deflection shapes be used in predicting flutter in place of vibrational shapes . if so, can we provide a justification by means of an example .
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65 does the boundary layer on a flat plate in a shear flow induce a pressure gradient .
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66 can the procedure of matching inner and outer solutions for a viscous flow problem be applied when the main stream is a shear flow .
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67 can series expansions be found for the boundary layer on a flat plate in a shear flow .
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68 what possible techniques are available for computing the injection distribution corresponding to an isothermal transpiration cooled hemisphere .
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69 what is known regarding asymptotic solutions to the exact boundary layer equations .
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70 previous solutions to the boundary layer similarity equations .
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71 experimental results on hypersonic viscous interaction .
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72 what has been done about viscous interactions in relatively low reynolds number flows, particularly at high mach numbers .
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73 what role does the effect of chemical reaction (particularly when out of equilibrium) play in the similitude laws governing hypersonic flows over slender aerodynamic bodies .
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74 how significant is the possible pressure of a dissociated free stream with respect to the realization of hypersonic simulation in high enthalpy wind tunnels .
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75 do the discrepancies among current analyses of the vorticity effect on stagnation-point heat transfer result primarily from the differences in the viscosity-temperature law assumed .
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76 how far can one trust the linear viscosity-temperature solution assumed in some of the analyses of hypersonic shock layer at low reynolds number .
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77 how close is the comparison of the shock layer theory with existing experiments in the low reynolds number (merged-layer) regime .
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78 has anyone explained the kink in the surge line of a multi-stage axial compressor .
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79 have any aerodynamic derivatives been measured at hypersonic mach numbers and comparison been made with theoretical work .
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80 are methods of measuring aerodynamic derivatives available which could be adopted for use in short running time facilities .
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81 what are wind-tunnel corrections for a two-dimensional aerofoil mounted off-centre in a tunnel .
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82 how do kuchemann's and multhopp's methods for calculating lift distributions on swept wings in subsonic flow compare with each other and with experiment .
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83 what is the present state of the theory of quasi-conical flows .
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84 references on the methods available for accurately estimating aerodynamic heat transfer to conical bodies for both laminar and turbulent flow .
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85 what parameters can seriously influence natural transition from laminar to turbulent flow on a model in a wind tunnel .
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86 can a satisfactory experimental technique be developed for measuring oscillatory derivatives on slender sting-mounted models in supersonic wind tunnels .
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87 what effect has the boundary layer in modifying the basic inviscid flow behind the shock, neglecting effects of leading edge and corner .
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88 how does a satellite orbit contract under the action of air drag in an atmosphere in which the scale height varies with altitude .
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89 how is the flow at transonic speeds about a delta wing different from that on a closely-related tapered sweptback wing .
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90 recent data on shock-induced boundary-layer separation .
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91 what interference effects are likely at transonic speeds .
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92 given complete freedom in the design of an airplane, what procedure would be used in order to minimize sonic boom intensity, and is there a limit to the degree of minimizing that can be accomplished .
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93 can methane-air combustion product be used as a hypersonic test medium and predict, within experimental accuracies, the results obtained in air .
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94 what is the theoretical heat transfer rate at the stagnation point of a blunt body .
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95 what is the theoretical heat transfer distribution around a hemisphere .
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96 has anyone investigated the unsteady lift distributions on finite wings in subsonic flow .
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97 what information is available for dynamic response of airplanes to gusts or blasts in the subsonic regime .
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98 will forward or apex located controls be effective at low subsonic speeds and how do they compare with conventional trailing-edge flaps .
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99 given that an uncontrolled vehicle will tumble as it enters an atmosphere, is it possible to predict when and how it will stop tumbling and its subsequent motion .
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100 what are the effects of initial imperfections on the elastic buckling of cylindrical shells under axial compression .
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101 why does the incremental theory and the deformation theory of plastic stress-strain relationship differ greatly when applied to stability problems .
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102 basic dynamic characteristics of structures continuous over many spans .
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103 is the information on the buckling of sandwich sphere available .
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104 can the load deformation characteristics of a beam be obtained with the material being inelastic and a non uniform temperature being present .
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105 what is the effect of an internal liquid column on the breathing vibrations of a cylindrical shell .
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106 experimental techniques in shell vibration .
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107 in summarizing theoretical and experimental work on the behaviour of a typical aircraft structure in a noise environment is it possible to develop a design procedure .
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108 what data is there on the fatigue of structures under acoustic loading .
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109 panels subjected to aerodynamic heating .
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110 can increasing the edge loading of a plate beyond the critical value for buckling change the buckling mode .
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111 have the effects of an elastic edge restraint been considered in previous papers on panel flutter .
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112 has the solution of the clamped plate problem, in the classical theory of bending, been reduced to two successive membrane boundary value problems .
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113 what data exists on oscillatory aerodynamic forces on control surfaces at transonic mach numbers .
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114 it is not likely that the airforces on a wing of general planform oscillating in transonic flow can be determined by purely analytical methods . is it possible to determine the airforces on a single particular planform, such as the rectangular one by such method .
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115 is the problem of similarity for representative investigations of aeroelastic effects in heated flow as intractable as previous investigations imply .
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116 what is the magnitude and distribution of lift over the cone and the cylindrical portion of a cone-cylinder configuration .
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117 is there any information on how the addition of a /boat-tail/ affects the normal force on the body of various angles of incidence .
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118 what are the aerodynamic interference effects on the fin lift and body lift of a fin-body combination .
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119 what is the effect of initial axisymmetric deviations from circularity on the non linear (large-deflection) load-deflection response of cylinders under hydrostatic pressure .
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120 are previous analyses of circumferential thermal buckling of circular cylindrical shells unnecessarily involved or even inaccurate due to the assumed forms of buckling mode .
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121 what papers are there dealing with circumferential buckling either thermal buckling or due to mechanical loading .
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122 what analytical investigations have been made of the stability of conical shells . how do the results compare with experiment .
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123 has any work been done on determining the nature of compressible viscous flow in a straight channel .
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124 in what areas, other than low density wind tunnel flows, is viscous compressible flow in slender channels a problem . what analytical investigations have been made of the stability of conical shells . how do the results compare with experiment .
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125 jet interference with supersonic flow -dash experimental papers .
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126 thrust vector control by fluid injection -dash papers .
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127 is it possible to obtain a reasonably simple analytical solution to the heat equation for an exponential (in time) heat input .
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128 has anyone programmed a pump design method for a high-speed digital computer .
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129 has anyone derived simplified pump design equation from the fundamental three-dimensional equations for incompressible nonviscous flow .
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130 what are the flutter characteristics of the exposed skin panels of the x-15 vertical stabilizer when subjected to aerodynamic heating .
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131 what agreement is found between theoretically predicted instability times and experimentally measured collapse times for compressed columns in creep .
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132 theoretical studies of creep buckling .
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133 experimental studies of creep buckling .
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134 is it possible to correlate the results on the creep buckling of widely different structures within the framework of a single theory .
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135 what are the experimental results for the creep buckling of columns .
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136 what are the results for the creep buckling of round tubes under external pressure .
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137 have any analytical studies been conducted on the time-to-failure mechanism associated with creep collapse for a long circular cylindrical shell which exhibits both primary and secondary creep as well as elastic deformations under various distributed force systems .
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138 has the effect of initial stresses, on the frequencies of vibration of circular cylindrical shells, been investigated .
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139 has the effect of the change of initial pressure due to deformation, on the frequencies of vibration of circular cylindrical shells been investigated .
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140 what are the discontinuity stresses at junctions in pressurized structures .
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141 what analytical solutions are available for stresses in edge-loaded shells of revolution .
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142 what dome contours minimize discontinuity stresses when used as closures on cylindrical pressure vessels .
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143 what general solutions for the stresses in pressurized shells of revolution are available .
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144 can studies of pure membrane cylinders having no wall bending stiffness but maintaining their shape by virtue of internal pressure provide any insight into the behaviour of pressurized cylinders with finite wall stiffness .
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145 what are the best experimental data and classical small deflection theory analyses available for pressurized cylinders in bending .
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146 does a membrane theory exist by which the behaviour of pressurized membrane cylinders in bending can be predicted .
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147 what are the equations which define the stability of simply supported corrugated core sandwich cylinders .
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148 papers on small deflection theory for buckling of sandwich cylinders .
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149 has anyone developed an analysis which accurately establishes the large deflection behaviour of conical shells .
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150 what is the magnitude of second-order wing-body interference at high supersonic mach number .
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151 what is the best theoretical method for calculating pressure on the surface of a wing alone .
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152 how can the effect of the boundary-layer on wing pressure be calculated, and what is its magnitude .
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153 how should the navier-stokes difference equations be solved .
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154 which iterative method for solving linear elliptic difference equations is most rapidly convergent .
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155 technical report on measurement of ablation during flight .
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156 what qualitative and quantitative material is available on ablation materials research .
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157 have flow fields been calculated for blunt-nosed bodies and compared with experiment for a wide range of free stream conditions and body shapes .
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158 what are the available properties of high-temperature air .
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159 what is the magnitude of aerodynamic damping in flexible vibration modes of a slender body of revolution characteristic of launch vehicles .
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160 compressive circumferential stresses in a torispherical shell reveal the possibility of buckling under internal pressure . has anyone investigated for which ranges of shell parameters these stresses are sufficiently large to cause elastic buckling .
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161 is there an integral method to give a single and sufficiently accurate method of calculating the laminar separate point for various incompressible and compressible boundary layers with zero heat transfer .
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162 what accurate or exact solutions of the laminar separation point for various incompressible and compressible boundary layers with zero heat transfer are available .
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163 can the hypersonic similarity results be applied to the technique of predicting surface pressures of an ogive forebody at angle of attack .
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164 what determines the onset of shock-induced boundary-layer separation .
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165 are the stable profiles of a compressible boundary layer induced by a moving wave known .
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166 are there experimental results on the stability of a compressible boundary layer induced by a moving wave .
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167 exact solution methods for calculating the ablative mass loss of a material ablating at high temperatures in a hypersonic flight environment .
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168 what approximate solutions are known to the direct problem of transonic flow in the throat of a nozzle, i.e. finding the flow in a given nozzle .
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169 what approximate solutions are known to the indirect problem of transonic flow in the throat of a nozzle, i.e. finding a nozzle which has a given axial velocity distribution .
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170 why do users of orthodox pitot-static tubes often find that the calibrations appear to be,. - (a) significantly different from those formerly specified, (b) wildly variable at low reynolds numbers .
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171 has a comparison been made between interference-free drag measurements using free-flight models and similar measurements made in a low-blockage wind tunnel .
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172 solution of the blasius problem with three-point boundary conditions .
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173 references on lyapunov's method on the stability of linear differential equations with periodic coefficients .
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174 obtain all papers and reports that contain shock detachment distance data .
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175 work on flow in channels at low reynolds numbers .
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176 some approximate analytical heat conduction solutions using methods other than biot's principle .
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177 what mode of stalling can be expected for each stage of an axial compressor .
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178 has a criterion been established for determining the axial compressor choking line .
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179 has a theory of quasi-conical flows been developed, in supersonic linearised theory, for which the upwash distribution on the lifting surface, apart from being a homogeneous function in the co-ordinate, is permitted to have a quite general functional form .
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180 how does scale height vary with altitude in an atmosphere .
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181 jet interference with supersonic flows theoretical papers .
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182 effects of leading-edge bluntness on the flutter characteristics of some square-planform double-wedge airfoils at mach numbers less than 15.4.
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183 what factors have been shown to have a primary influence on sonic boom strength .
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184 work on small-oscillation re-entry motions .
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185 experimental studies on panel flutter .
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186 how can wing-body, flow field interference effects be approximated rationally .
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187 has anyone analytically or experimentally investigated the effects of internal pressure on the buckling of circular-cylindrical shells under bending .
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188 what theoretical and experimental work has been done on the excitation and response of typical structures in a noise environment .
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189 is there a design method for calculating thermal fatigue endurances of components of various types and sizes in a variety of circumstances .
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190 will an analysis of panel flutter based on arbitrarily assumed modes of deformation prove satisfactory, and if so, what is the minimum number of modes that need be considered .
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191 what is the criterion for true panel flutter, as opposed to small amplitude vibration arising from acoustic disturbances .
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192 papers dealing with uniformly loaded sectors .
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193 general methods of solving clamped plate problems .
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194 how can the analytical solution of the buckling strength of a uniform circular cylinder loaded in axial compression be refined so as to lower the buckling load .
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195 in the problem of the buckling strength of uniform circular cylinders loaded in axial compression, does the linear solution help with improving the non-linear one .
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196 the problem of similarity for representative investigation of aeroelastic effects in a flow with the absence of heating effects .
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197 how is fatigue damage estimated using the normal long-hand method .
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198 is there any information available on the difference in the effects of various edge conditions on the buckling of cylindrical shells .
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199 have non-linear large deflection analyses been conducted for shell shapes other than conical .
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200 are asymptotic methods sufficiently accurate in the determination of pre-buckling stresses in torispherical shells, or must we resort to numerical methods .
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201 what are the nonequilibrium chemical constituents in the viscous shock layer ahead of a blunt re-entry vehicle .
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202 how accurate are existing analytical theories in estimating pressure distributions on cones at incidence, at hypersonic speeds .
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203 are simple empirical methods of any use for estimating pressure distribution in cones .
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204 do viscous effects seriously modify pressure distributions .
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205 has anyone investigated theoretically whether surface flexibility can stabilize a laminar boundary layer .
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206 how do subsonic and transonic flutter data measured in the new langley transonic dynamics tunnel compare with similar data obtained in other facilities .
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207 how do large changes in new mass ratio quantitatively affect wing-flutter boundaries .
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208 what is the effect of the shape of the drag polar of a lifting spacecraft on the amount of reduction in maximum deceleration obtainable by continuously varying the aerodynamic coefficients during re-entry .
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209 what are the physical significance and characteristics of separated laminar and turbulent boundary layer flows .
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210 has anyone analytically investigated the stabilizing influence of soft elastic cores on the buckling strength of cylindrical shells subjected to non-uniform external pressure .
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211 what papers are available on the buckling of empty cylindrical shells under non-uniform pressure .
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212 what effect do thermal stresses have on the compressive buckling strength of ring-stiffened cylinders .
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213 what is the effect on cylinder buckling of a circumferential stress system that varies in the axial direction .
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214 can non-linear shallow shell analysis be reduced to an engineering technique by use of the matrix .
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215 is it possible to predict the shape of a shroud which will allow simulation of the nose region flow field for a sphere in hypersonic flow .
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216 what investigations have been made of the wave system created by a static pressure distribution over a liquid surface .
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217 has anyone investigated the effect of shock generated vorticity on heat transfer to a blunt body .
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218 what is the heat transfer to a blunt body in the absence of vorticity .
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219 what are the general effects on flow fields when the reynolds number is small .
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220 find a calculation procedure applicable to all incompressible laminar boundary layer flow problems having good accuracy and reasonable computation time .
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221 papers applicable to this problem (calculation procedures for laminar incompressible flow with arbitrary pressure gradient) .
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222 has anyone investigated the shear buckling of stiffened plates .
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223 papers on shear buckling of unstiffened rectangular plates under shear .
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224 in practice, how close to reality are the assumptions that the flow in a hypersonic shock tube using nitrogen is non-viscous and in thermodynamic equilibrium .
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225 what design factors can be used to control lift-drag ratios at mach numbers above 5 .
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@ -7,7 +7,7 @@ OUT="results.txt"
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DATASET="cranfield"
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QUERY="cran"
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STOPWORDS="english"
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MODE="duckdb"
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MODE="phrases"
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CODE="phrase_index.py"
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EXTRACTOR="phrases_extractor.py"
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LIMIT=-1
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@ -23,6 +23,7 @@ MIN_PMI=4.0
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RUN_ID=$(date +"%Y%m%d_%H%M%S")
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RESULTS_DIR="results/$RUN_ID"
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cd ..
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# Step 1: Build the index
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python $CODE --db "$DB" --dataset "$DATASET" --stopwords "$STOPWORDS" --mode "$MODE" --limit "$LIMIT" --min-freq "$MIN_FREQ" --min-pmi "$MIN_PMI"
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@ -3,6 +3,7 @@ set -e
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DB_BASE="database"
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OUT_BASE="results"
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RESULTS_BASE="results_new_postings"
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DATASET="cranfield"
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QUERY="cran"
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INDEXER="phrase_index.py"
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@ -10,8 +11,8 @@ INDEXER="phrase_index.py"
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STOPWORDS_LIST=("english" "none")
|
||||
MODE_LIST=("duckdb" "phrases")
|
||||
LIMIT_LIST=(-1)
|
||||
MIN_FREQ_LIST=(4 5 6 7 9 10 11)
|
||||
MIN_PMI_LIST=(5 6 7 8 9 10 11 12 13 14)
|
||||
MIN_FREQ_LIST=(0 1 2 4 5 6 7 8 9 10 11 16 24 48)
|
||||
MIN_PMI_LIST=(0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 24 48)
|
||||
|
||||
cd ..
|
||||
|
||||
@ -34,7 +35,7 @@ for STOPWORDS in "${STOPWORDS_LIST[@]}"; do
|
||||
|
||||
# Timestamped results directory
|
||||
RUN_ID=$(date +"%Y%m%d_%H%M%S")_${MODE}_${STOPWORDS}_${LIMIT}_${MIN_FREQ}_${MIN_PMI}
|
||||
RESULTS_DIR="results/$RUN_ID"
|
||||
RESULTS_DIR="$RESULTS_BASE/$RUN_ID"
|
||||
mkdir -p "$RESULTS_DIR"
|
||||
|
||||
# Step 1: Build the index
|
||||
|
||||
@ -2,7 +2,7 @@
|
||||
|
||||
echo -e "RUN_ID\tMODE\tSTOPWORDS\tMIN_FREQ\tMIN_PMI\tMAP\tPOSTINGS_COST\tDICT_SIZE\tTERMS_SIZE\tNGRAMS\tAVGDL\tSUMDF"
|
||||
|
||||
for dir in ../results/*; do
|
||||
for dir in ../results_new_postings/*; do
|
||||
[ -d "$dir" ] || continue
|
||||
SETTINGS="$dir/settings.txt"
|
||||
EVAL="$dir/eval.txt"
|
||||
|
||||
563
helper_scripts/output_new_postings.csv
Normal file
563
helper_scripts/output_new_postings.csv
Normal file
@ -0,0 +1,563 @@
|
||||
RUN_ID MODE STOPWORDS MIN_FREQ MIN_PMI MAP POSTINGS_COST DICT_SIZE TERMS_SIZE NGRAMS AVGDL SUMDF
|
||||
20250821_151309_duckdb_english_-1_0_0 duckdb english 0 0 0.2881 1186.5289 6639 128030 0 91.45 80317
|
||||
20250821_151346_phrases_english_-1_0_0 phrases english 0 0 0.1572 615.7689 21928 102342 16988 73.10142857142857 77971
|
||||
20250821_151545_phrases_english_-1_0_1 phrases english 0 1 0.1629 647.7733 21685 102526 16746 73.23285714285714 77793
|
||||
20250821_151754_phrases_english_-1_0_2 phrases english 0 2 0.1688 679.1822 21052 103046 16109 73.60428571428571 77506
|
||||
20250821_152001_phrases_english_-1_0_3 phrases english 0 3 0.1669 720.2044 20102 104132 15148 74.38 77606
|
||||
20250821_152210_phrases_english_-1_0_4 phrases english 0 4 0.1778 785.1689 18662 106284 13680 75.91714285714286 77921
|
||||
20250821_152408_phrases_english_-1_0_5 phrases english 0 5 0.1905 898.9511 16899 109637 11883 78.31214285714286 78641
|
||||
20250821_152601_phrases_english_-1_0_6 phrases english 0 6 0.2069 1043.4444 14860 114007 9804 81.43357142857143 79598
|
||||
20250821_152749_phrases_english_-1_0_7 phrases english 0 7 0.2339 1188.9200 12928 119090 7820 85.06428571428572 80545
|
||||
20250821_152913_phrases_english_-1_0_8 phrases english 0 8 0.2568 1361.3689 11156 126009 5981 90.00642857142857 82155
|
||||
20250821_153053_phrases_english_-1_0_9 phrases english 0 9 0.2719 1437.9778 9605 130791 4290 93.42214285714286 83560
|
||||
20250821_153226_phrases_english_-1_0_10 phrases english 0 10 0.2820 1467.1689 8539 133875 2996 95.625 84619
|
||||
20250821_153351_phrases_english_-1_0_11 phrases english 0 11 0.2849 1475.1244 7730 135702 2010 96.93 85361
|
||||
20250821_153515_phrases_english_-1_0_12 phrases english 0 12 0.2890 1478.2444 7220 136986 1305 97.84714285714286 85910
|
||||
20250821_153639_phrases_english_-1_0_13 phrases english 0 13 0.2919 1472.1511 6885 137827 779 98.44785714285715 86301
|
||||
20250821_153752_phrases_english_-1_0_14 phrases english 0 14 0.2911 1472.6711 6714 138289 451 98.77785714285714 86539
|
||||
20250821_153909_phrases_english_-1_0_15 phrases english 0 15 0.2907 1472.7422 6627 138579 258 98.985 86697
|
||||
20250821_154022_phrases_english_-1_0_16 phrases english 0 16 0.2906 1472.8756 6593 138733 129 99.095 86796
|
||||
20250821_154138_phrases_english_-1_0_17 phrases english 0 17 0.2906 1472.9111 6598 138829 44 99.16357142857143 86872
|
||||
20250821_154243_phrases_english_-1_0_24 phrases english 0 24 0.2906 1472.9200 6639 138873 0 99.195 86916
|
||||
20250821_154350_phrases_english_-1_0_48 phrases english 0 48 0.2906 1472.9200 6639 138873 0 99.195 86916
|
||||
20250821_154453_phrases_english_-1_1_0 phrases english 1 0 0.1572 615.7689 21928 102342 16988 73.10142857142857 77971
|
||||
20250821_154658_phrases_english_-1_1_1 phrases english 1 1 0.1629 647.7733 21685 102526 16746 73.23285714285714 77793
|
||||
20250821_154907_phrases_english_-1_1_2 phrases english 1 2 0.1688 679.1822 21052 103046 16109 73.60428571428571 77506
|
||||
20250821_155115_phrases_english_-1_1_3 phrases english 1 3 0.1669 720.2044 20102 104132 15148 74.38 77606
|
||||
20250821_155322_phrases_english_-1_1_4 phrases english 1 4 0.1778 785.1689 18662 106284 13680 75.91714285714286 77921
|
||||
20250821_155521_phrases_english_-1_1_5 phrases english 1 5 0.1905 898.9511 16899 109637 11883 78.31214285714286 78641
|
||||
20250821_155649_phrases_english_-1_1_6 phrases english 1 6 0.2069 1043.4444 14860 114007 9804 81.43357142857143 79598
|
||||
20250821_155840_phrases_english_-1_1_7 phrases english 1 7 0.2339 1188.9200 12928 119090 7820 85.06428571428572 80545
|
||||
20250821_160021_phrases_english_-1_1_8 phrases english 1 8 0.2568 1361.3689 11156 126009 5981 90.00642857142857 82155
|
||||
20250821_160158_phrases_english_-1_1_9 phrases english 1 9 0.2719 1437.9778 9605 130791 4290 93.42214285714286 83560
|
||||
20250821_160317_phrases_english_-1_1_10 phrases english 1 10 0.2820 1467.1689 8539 133875 2996 95.625 84619
|
||||
20250821_160446_phrases_english_-1_1_11 phrases english 1 11 0.2849 1475.1244 7730 135702 2010 96.93 85361
|
||||
20250821_160604_phrases_english_-1_1_12 phrases english 1 12 0.2890 1478.2444 7220 136986 1305 97.84714285714286 85910
|
||||
20250821_160725_phrases_english_-1_1_13 phrases english 1 13 0.2919 1472.1511 6885 137827 779 98.44785714285715 86301
|
||||
20250821_160840_phrases_english_-1_1_14 phrases english 1 14 0.2911 1472.6711 6714 138289 451 98.77785714285714 86539
|
||||
20250821_160959_phrases_english_-1_1_15 phrases english 1 15 0.2907 1472.7422 6627 138579 258 98.985 86697
|
||||
20250821_161116_phrases_english_-1_1_16 phrases english 1 16 0.2906 1472.8756 6593 138733 129 99.095 86796
|
||||
20250821_161232_phrases_english_-1_1_17 phrases english 1 17 0.2906 1472.9111 6598 138829 44 99.16357142857143 86872
|
||||
20250821_161344_phrases_english_-1_1_24 phrases english 1 24 0.2906 1472.9200 6639 138873 0 99.195 86916
|
||||
20250821_161455_phrases_english_-1_1_48 phrases english 1 48 0.2906 1472.9200 6639 138873 0 99.195 86916
|
||||
20250821_161601_phrases_english_-1_2_0 phrases english 2 0 0.1763 481.4044 10740 105739 6586 75.52785714285714 79664
|
||||
20250821_161715_phrases_english_-1_2_1 phrases english 2 1 0.1772 505.9111 10666 105816 6512 75.58285714285714 79489
|
||||
20250821_161827_phrases_english_-1_2_2 phrases english 2 2 0.1794 532.6844 10427 106096 6273 75.78285714285714 79150
|
||||
20250821_161940_phrases_english_-1_2_3 phrases english 2 3 0.1810 568.5600 10036 106808 5881 76.29142857142857 79059
|
||||
20250821_162106_phrases_english_-1_2_4 phrases english 2 4 0.1938 622.4844 9433 108408 5271 77.43428571428572 79099
|
||||
20250821_162231_phrases_english_-1_2_5 phrases english 2 5 0.1992 731.1289 8641 111018 4475 79.29857142857144 79410
|
||||
20250821_162353_phrases_english_-1_2_6 phrases english 2 6 0.2151 867.9867 7697 114500 3528 81.78571428571429 79898
|
||||
20250821_162515_phrases_english_-1_2_7 phrases english 2 7 0.2441 1007.2267 6857 118615 2684 84.725 80372
|
||||
20250821_162628_phrases_english_-1_2_8 phrases english 2 8 0.2627 1173.8622 6083 124639 1908 89.02785714285714 81508
|
||||
20250821_162739_phrases_english_-1_2_9 phrases english 2 9 0.2718 1245.7244 5438 128486 1240 91.77571428571429 82376
|
||||
20250821_162849_phrases_english_-1_2_10 phrases english 2 10 0.2806 1271.9556 5049 130739 821 93.385 82993
|
||||
20250821_163000_phrases_english_-1_2_11 phrases english 2 11 0.2852 1277.9422 4732 131933 492 94.23785714285714 83368
|
||||
20250821_163112_phrases_english_-1_2_12 phrases english 2 12 0.2915 1279.8844 4564 132722 294 94.80142857142857 83603
|
||||
20250821_163223_phrases_english_-1_2_13 phrases english 2 13 0.2941 1280.1644 4440 133189 151 95.135 83759
|
||||
20250821_163332_phrases_english_-1_2_14 phrases english 2 14 0.2931 1280.4222 4390 133396 83 95.28285714285714 83832
|
||||
20250821_163440_phrases_english_-1_2_15 phrases english 2 15 0.2932 1280.4444 4356 133545 34 95.38928571428572 83881
|
||||
20250821_163545_phrases_english_-1_2_16 phrases english 2 16 0.2932 1280.4533 4347 133593 12 95.42357142857144 83902
|
||||
20250821_163650_phrases_english_-1_2_17 phrases english 2 17 0.2932 1280.4533 4349 133616 0 95.44 83913
|
||||
20250821_163755_phrases_english_-1_2_24 phrases english 2 24 0.2932 1280.4533 4349 133616 0 95.44 83913
|
||||
20250821_163900_phrases_english_-1_2_48 phrases english 2 48 0.2932 1280.4533 4349 133616 0 95.44 83913
|
||||
20250821_164005_phrases_english_-1_4_0 phrases english 4 0 0.1926 532.7511 5392 108052 2439 77.18 77560
|
||||
20250821_164113_phrases_english_-1_4_1 phrases english 4 1 0.1954 549.7644 5376 108073 2423 77.195 77458
|
||||
20250821_164221_phrases_english_-1_4_2 phrases english 4 2 0.1955 566.2400 5305 108193 2352 77.28071428571428 77205
|
||||
20250821_164328_phrases_english_-1_4_3 phrases english 4 3 0.1990 594.6533 5184 108612 2231 77.58 77121
|
||||
20250821_164440_phrases_english_-1_4_4 phrases english 4 4 0.2077 634.6889 4969 109698 2015 78.35571428571428 77107
|
||||
20250821_164552_phrases_english_-1_4_5 phrases english 4 5 0.2083 729.8622 4654 111616 1700 79.72571428571429 77189
|
||||
20250821_164704_phrases_english_-1_4_6 phrases english 4 6 0.2195 863.5956 4250 114239 1297 81.59928571428571 77437
|
||||
20250821_164812_phrases_english_-1_4_7 phrases english 4 7 0.2465 994.1956 3904 117509 950 83.935 77710
|
||||
20250821_164920_phrases_english_-1_4_8 phrases english 4 8 0.2703 1157.7733 3584 122735 630 87.66785714285714 78610
|
||||
20250821_165029_phrases_english_-1_4_9 phrases english 4 9 0.2796 1224.1600 3346 125792 390 89.85142857142857 79288
|
||||
20250821_165136_phrases_english_-1_4_10 phrases english 4 10 0.2870 1248.1289 3205 127524 245 91.08857142857143 79810
|
||||
20250821_165242_phrases_english_-1_4_11 phrases english 4 11 0.2910 1252.4222 3106 128280 141 91.62857142857143 80077
|
||||
20250821_165349_phrases_english_-1_4_12 phrases english 4 12 0.2940 1254.0400 3044 128816 74 92.01142857142857 80251
|
||||
20250821_165453_phrases_english_-1_4_13 phrases english 4 13 0.2948 1254.5600 3006 129079 34 92.19928571428571 80351
|
||||
20250821_165558_phrases_english_-1_4_14 phrases english 4 14 0.2938 1254.6400 2989 129185 14 92.275 80400
|
||||
20250821_165701_phrases_english_-1_4_15 phrases english 4 15 0.2938 1254.6578 2981 129248 2 92.32 80420
|
||||
20250821_165805_phrases_english_-1_4_16 phrases english 4 16 0.2938 1254.6578 2980 129255 0 92.325 80420
|
||||
20250821_165906_phrases_english_-1_4_17 phrases english 4 17 0.2938 1254.6578 2980 129255 0 92.325 80420
|
||||
20250821_170006_phrases_english_-1_4_24 phrases english 4 24 0.2938 1254.6578 2980 129255 0 92.325 80420
|
||||
20250821_170109_phrases_english_-1_4_48 phrases english 4 48 0.2938 1254.6578 2980 129255 0 92.325 80420
|
||||
20250821_170210_phrases_english_-1_5_0 phrases english 5 0 0.2001 543.2089 4365 108248 1765 77.32 76546
|
||||
20250821_170321_phrases_english_-1_5_1 phrases english 5 1 0.2026 559.7600 4352 108267 1752 77.33357142857143 76440
|
||||
20250821_170431_phrases_english_-1_5_2 phrases english 5 2 0.2037 573.0400 4304 108355 1704 77.39642857142857 76213
|
||||
20250821_170537_phrases_english_-1_5_3 phrases english 5 3 0.2056 596.1200 4228 108681 1628 77.62928571428571 76144
|
||||
20250821_170644_phrases_english_-1_5_4 phrases english 5 4 0.2156 634.8933 4068 109670 1468 78.33571428571429 76123
|
||||
20250821_170757_phrases_english_-1_5_5 phrases english 5 5 0.2173 725.4356 3835 111400 1235 79.57142857142857 76183
|
||||
20250821_170908_phrases_english_-1_5_6 phrases english 5 6 0.2309 857.5511 3536 113742 936 81.24428571428571 76390
|
||||
20250821_171021_phrases_english_-1_5_7 phrases english 5 7 0.2538 984.3911 3280 116753 680 83.395 76603
|
||||
20250821_171130_phrases_english_-1_5_8 phrases english 5 8 0.2713 1145.1200 3035 121771 435 86.97928571428571 77476
|
||||
20250821_171244_phrases_english_-1_5_9 phrases english 5 9 0.2818 1208.6000 2870 124598 270 88.99857142857142 78102
|
||||
20250821_171401_phrases_english_-1_5_10 phrases english 5 10 0.2888 1232.2356 2768 126202 166 90.14428571428572 78608
|
||||
20250821_171511_phrases_english_-1_5_11 phrases english 5 11 0.2923 1236.3244 2702 126846 97 90.60428571428571 78836
|
||||
20250821_171623_phrases_english_-1_5_12 phrases english 5 12 0.2926 1237.8311 2656 127310 49 90.93571428571428 79002
|
||||
20250821_171734_phrases_english_-1_5_13 phrases english 5 13 0.2940 1238.1689 2632 127516 23 91.08285714285714 79084
|
||||
20250821_171844_phrases_english_-1_5_14 phrases english 5 14 0.2936 1238.2400 2621 127595 10 91.13928571428572 79117
|
||||
20250821_171954_phrases_english_-1_5_15 phrases english 5 15 0.2935 1238.2578 2615 127645 1 91.175 79132
|
||||
20250821_172103_phrases_english_-1_5_16 phrases english 5 16 0.2935 1238.2578 2614 127648 0 91.17714285714285 79131
|
||||
20250821_172207_phrases_english_-1_5_17 phrases english 5 17 0.2935 1238.2578 2614 127648 0 91.17714285714285 79131
|
||||
20250821_172308_phrases_english_-1_5_24 phrases english 5 24 0.2935 1238.2578 2614 127648 0 91.17714285714285 79131
|
||||
20250821_172410_phrases_english_-1_5_48 phrases english 5 48 0.2935 1238.2578 2614 127648 0 91.17714285714285 79131
|
||||
20250821_172511_phrases_english_-1_6_0 phrases english 6 0 0.2187 592.0533 3704 108857 1354 77.755 75943
|
||||
20250821_172620_phrases_english_-1_6_1 phrases english 6 1 0.2199 602.5467 3696 108863 1346 77.75928571428571 75853
|
||||
20250821_172728_phrases_english_-1_6_2 phrases english 6 2 0.2200 612.0844 3664 108937 1314 77.81214285714286 75682
|
||||
20250821_172837_phrases_english_-1_6_3 phrases english 6 3 0.2218 630.9511 3609 109185 1259 77.98928571428571 75616
|
||||
20250821_172945_phrases_english_-1_6_4 phrases english 6 4 0.2300 667.9333 3490 110059 1140 78.61357142857143 75586
|
||||
20250821_173055_phrases_english_-1_6_5 phrases english 6 5 0.2286 752.7378 3326 111572 976 79.69428571428571 75634
|
||||
20250821_173203_phrases_english_-1_6_6 phrases english 6 6 0.2452 876.2889 3090 113712 740 81.22285714285714 75810
|
||||
20250821_173311_phrases_english_-1_6_7 phrases english 6 7 0.2606 1000.4489 2883 116571 533 83.265 76015
|
||||
20250821_173420_phrases_english_-1_6_8 phrases english 6 8 0.2758 1157.8800 2686 121408 336 86.72 76833
|
||||
20250821_173529_phrases_english_-1_6_9 phrases english 6 9 0.2832 1219.9778 2556 124095 206 88.63928571428572 77428
|
||||
20250821_173639_phrases_english_-1_6_10 phrases english 6 10 0.2871 1243.9600 2468 125638 116 89.74142857142857 77916
|
||||
20250821_173744_phrases_english_-1_6_11 phrases english 6 11 0.2896 1247.6356 2417 126211 64 90.15071428571429 78124
|
||||
20250821_173850_phrases_english_-1_6_12 phrases english 6 12 0.2913 1249.0978 2382 126624 27 90.44571428571429 78278
|
||||
20250821_173954_phrases_english_-1_6_13 phrases english 6 13 0.2927 1249.4178 2366 126799 9 90.57071428571429 78352
|
||||
20250821_174055_phrases_english_-1_6_14 phrases english 6 14 0.2928 1249.4178 2362 126842 4 90.60142857142857 78373
|
||||
20250821_174202_phrases_english_-1_6_15 phrases english 6 15 0.2927 1249.4267 2359 126869 0 90.62071428571429 78376
|
||||
20250821_174303_phrases_english_-1_6_16 phrases english 6 16 0.2927 1249.4267 2359 126869 0 90.62071428571429 78376
|
||||
20250821_174405_phrases_english_-1_6_17 phrases english 6 17 0.2927 1249.4267 2359 126869 0 90.62071428571429 78376
|
||||
20250821_174506_phrases_english_-1_6_24 phrases english 6 24 0.2927 1249.4267 2359 126869 0 90.62071428571429 78376
|
||||
20250821_174605_phrases_english_-1_6_48 phrases english 6 48 0.2927 1249.4267 2359 126869 0 90.62071428571429 78376
|
||||
20250821_174706_phrases_english_-1_7_0 phrases english 7 0 0.2257 620.9244 3223 109292 1073 78.06571428571428 75469
|
||||
20250821_174816_phrases_english_-1_7_1 phrases english 7 1 0.2270 631.0978 3220 109292 1070 78.06571428571428 75375
|
||||
20250821_174926_phrases_english_-1_7_2 phrases english 7 2 0.2266 641.2000 3197 109357 1047 78.11214285714286 75242
|
||||
20250821_175037_phrases_english_-1_7_3 phrases english 7 3 0.2283 659.9422 3154 109572 1004 78.26571428571428 75177
|
||||
20250821_175144_phrases_english_-1_7_4 phrases english 7 4 0.2362 695.0933 3060 110363 910 78.83071428571428 75134
|
||||
20250821_175252_phrases_english_-1_7_5 phrases english 7 5 0.2358 778.1289 2934 111748 784 79.82 75148
|
||||
20250821_175400_phrases_english_-1_7_6 phrases english 7 6 0.2455 887.6400 2748 113674 598 81.19571428571429 75290
|
||||
20250821_175508_phrases_english_-1_7_7 phrases english 7 7 0.2617 1008.7733 2577 116381 427 83.12928571428571 75452
|
||||
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|
||||
20250823_155407_phrases_none_-1_48_12 phrases none 48 12 0.2526 14132.6800 703 344009 0 245.72071428571428 110182
|
||||
20250823_155506_phrases_none_-1_48_13 phrases none 48 13 0.2526 14132.6800 703 344009 0 245.72071428571428 110182
|
||||
20250823_155605_phrases_none_-1_48_14 phrases none 48 14 0.2526 14132.6800 703 344009 0 245.72071428571428 110182
|
||||
20250823_155702_phrases_none_-1_48_15 phrases none 48 15 0.2526 14132.6800 703 344009 0 245.72071428571428 110182
|
||||
20250823_155759_phrases_none_-1_48_16 phrases none 48 16 0.2526 14132.6800 703 344009 0 245.72071428571428 110182
|
||||
20250823_155857_phrases_none_-1_48_17 phrases none 48 17 0.2526 14132.6800 703 344009 0 245.72071428571428 110182
|
||||
20250823_155955_phrases_none_-1_48_24 phrases none 48 24 0.2526 14132.6800 703 344009 0 245.72071428571428 110182
|
||||
20250823_160055_phrases_none_-1_48_48 phrases none 48 48 0.2526 14132.6800 703 344009 0 245.72071428571428 110182
|
||||
|
46
lm.sql
Normal file
46
lm.sql
Normal file
@ -0,0 +1,46 @@
|
||||
CREATE OR REPLACE MACRO fts_main_documents.match_lm(query_string, fields := NULL, lambda := 0.3, conjunctive := 0) AS TABLE (
|
||||
WITH tokens AS (
|
||||
SELECT DISTINCT stem(unnest(fts_main_documents.tokenize(query_string)), 'none') AS t
|
||||
),
|
||||
fieldids AS (
|
||||
SELECT fieldid
|
||||
FROM fts_main_documents.fields
|
||||
WHERE CASE WHEN ((fields IS NULL)) THEN (1) ELSE (field = ANY(SELECT * FROM (SELECT unnest(string_split(fields, ','))) AS fsq)) END
|
||||
),
|
||||
qtermids AS (
|
||||
SELECT termid, df
|
||||
FROM fts_main_documents.dict AS dict, tokens
|
||||
WHERE (dict.term = tokens.t)
|
||||
),
|
||||
qterms AS (
|
||||
SELECT termid, docid
|
||||
FROM fts_main_documents.terms AS terms
|
||||
WHERE (CASE WHEN ((fields IS NULL)) THEN (1) ELSE (fieldid = ANY(SELECT * FROM fieldids)) END
|
||||
AND (termid = ANY(SELECT qtermids.termid FROM qtermids)))
|
||||
),
|
||||
term_tf AS (
|
||||
SELECT termid, docid, count_star() AS tf
|
||||
FROM qterms
|
||||
GROUP BY docid, termid
|
||||
),
|
||||
cdocs AS (
|
||||
SELECT docid
|
||||
FROM qterms
|
||||
GROUP BY docid
|
||||
HAVING CASE WHEN (conjunctive) THEN ((count(DISTINCT termid) = (SELECT count_star() FROM tokens))) ELSE 1 END
|
||||
),
|
||||
subscores AS (
|
||||
SELECT docs.docid, docs.len AS doc_len, term_tf.termid, term_tf.tf, qtermids.df, LN(1 + (lambda * tf * (SELECT ANY_VALUE(sumdf) FROM fts_main_documents.stats)) / ((1-lambda) * df * docs.len)) AS subscore
|
||||
FROM term_tf, cdocs, fts_main_documents.docs AS docs, qtermids
|
||||
WHERE ((term_tf.docid = cdocs.docid)
|
||||
AND (term_tf.docid = docs.docid)
|
||||
AND (term_tf.termid = qtermids.termid))
|
||||
),
|
||||
scores AS (
|
||||
SELECT docs.name AS docname, LN(MAX(doc_len)) + sum(subscore) AS score FROM subscores, fts_main_documents.docs AS docs WHERE subscores.docid = docs.docid GROUP BY docs.name
|
||||
),
|
||||
postings_cost AS (
|
||||
SELECT COUNT(*) AS cost FROM term_tf
|
||||
)
|
||||
SELECT docname, score, (SELECT cost FROM postings_cost) AS postings_cost FROM scores
|
||||
);
|
||||
@ -83,7 +83,7 @@ def create_lm(con, stemmer):
|
||||
SELECT docs.name AS docname, LN(MAX(doc_len)) + sum(subscore) AS score FROM subscores, fts_main_documents.docs AS docs WHERE subscores.docid = docs.docid GROUP BY docs.name
|
||||
),
|
||||
postings_cost AS (
|
||||
SELECT COUNT(DISTINCT docid) AS cost FROM qterms
|
||||
SELECT COUNT(*) AS cost FROM term_tf
|
||||
)
|
||||
SELECT docname, score, (SELECT cost FROM postings_cost) AS postings_cost FROM scores
|
||||
);
|
||||
|
||||
Loading…
Reference in New Issue
Block a user