Upload qrels (1).csv

qrels (1).csv

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+query_id,query,relevant_docs_gt_0
+1,"what similarity laws must be obeyed when constructing aeroelastic models
+of heated high speed aircraft .","['184', '29', '31', '12', '51', '102', '13', '14', '15', '57', '378', '859', '185', '30', '37', '52', '142', '195', '875', '56', '66', '95', '462', '497', '858', '876', '879', '880']"
+2,"what are the structural and aeroelastic problems associated with flight
+of high speed aircraft .","['12', '15', '184', '858', '51', '102', '202', '14', '52', '380', '746', '859', '948', '285', '390', '391', '442', '497', '643', '856', '857', '877', '864', '658']"
+4,"what problems of heat conduction in composite slabs have been solved so
+far .","['236', '166']"
+8,"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 .","['48', '122', '20', '58', '196', '354', '360', '197', '999', '1112', '1005']"
+9,"what chemical kinetic system is applicable to hypersonic aerodynamic
+problems .","['21', '22', '550']"
+10,"what theoretical and experimental guides do we have as to turbulent
+couette flow behaviour .","['259', '405', '302', '436', '437', '438', '998', '1011']"
+12,"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 .","['86', '194', '650', '649', '652']"
+13,"what methods -dash exact or approximate -dash are presently available
+for predicting body pressures at angle of attack.","['64', '265', '65', '311']"
+15,papers on internal /slip flow/ heat transfer studies .,"['463', '462']"
+18,"are real-gas transport properties for air available over a wide range of
+enthalpies and densities .","['196', '197', '198']"
+22,"is it possible to find an analytical,  similar solution of the strong
+blast wave problem in the newtonian approximation .",['68']
+23,"how can the aerodynamic performance of channel flow ground effect
+machines be calculated .","['900', '902', '200', '201', '601', '899', '903', '593', '199', '594', '901', '544', '597', '749', '917', '919', '1333', '634', '687', '698', '1290', '700', '704', '705', '1109', '1112', '1141', '1197', '1256', '1259', '1272', '1289']"
+26,what is the basic mechanism of the transonic aileron buzz .,"['145', '611', '376', '406', '565', '1076']"
+27,papers on shock-sound wave interaction .,"['224', '278', '428']"
+29,material properties of photoelastic materials .,"['250', '514', '609', '225', '793', '464', '465', '612', '466']"
+31,"can the transverse potential flow about a body of revolution be
+calculated efficiently by an electronic computer .",['776']
+32,"can the three-dimensional problem of a transverse potential flow about
+a body of revolution be reduced to a two-dimensional problem .","['465', '249', '777', '778', '247', '250']"
+33,"are experimental pressure distributions on bodies of revolution at angle
+of attack available .","['252', '431', '141']"
+34,"does there exist a good basic treatment of the dynamics of re-entry
+combining consideration of realistic effects with relative simplicity of
+results .","['252', '431', '672', '714', '799', '800']"
+35,"has anyone formally determined the influence of joule heating,  produced
+by the induced current,  in magnetohydrodynamic free convection flows
+under general conditions .","['166', '167', '132']"
+39,"why does the compressibility transformation fail to correlate the high
+speed data for helium and air .","['272', '555', '24', '283', '552', '79', '207', '418', '557', '554', '556', '505', '1257']"
+40,"did anyone else discover that the turbulent skin friction is not over
+sensitive to the nature of the variation of the viscosity with
+temperature .","['24', '283', '552', '272', '85', '976', '557', '558', '553', '554', '555', '556']"
+41,what progress has been made in research on unsteady aerodynamics .,"['288', '289', '433']"
+49,"what are the factors which influence the time required to invert large
+structural matrices .","['320', '478']"
+50,"does a practical flow follow the theoretical concepts for the
+interaction between adjacent blade rows of a supersonic cascade .","['326', '629', '21', '94', '22', '306']"
+51,"what is a single approximate formula for the displacement thickness of
+a laminar boundary layer in compressible flow on a flat plate .","['94', '23', '105', '381', '192', '326', '63', '494', '629', '261']"
+52,"how is the design of ring or part ring wings by linear theory affected
+by thickness .","['21', '22', '306', '326']"
+53,what application has the linear theory design of curved wings .,"['296', '33', '446', '447', '448', '449', '208', '297', '298', '299']"
+54,"what is the effect of cross sectional shape on the flow over simple
+delta wings with sharp leading edges .","['84', '24', '101', '294', '628', '661', '364', '365', '560']"
+55,papers on flow visualization on slender conical wings .,"['16', '375', '460', '378', '255', '271', '376', '377', '562', '502']"
+56,"what size of end plate can be safely used to simulate two-dimensional
+flow conditions over a bluff cylindrical body of finite aspect ratio .","['380', '749', '1339', '14', '705', '779', '780', '379', '643', '686']"
+57,"to find an approximate correction for thickness in slender thin-wing
+theory .","['380', '593', '746', '914', '14', '379', '705', '779', '780', '704', '12', '15', '857', '859']"
+58,"how do interference-free longitudinal stability measurements (made
+using free-flight models) compare with similar measurements made in
+a low-blockage wind tunnel .","['788', '785', '786', '787', '23', '381', '382', '784', '789']"
+59,"have wind tunnel interference effects been investigated on a systematic
+basis .","['788', '785', '786', '787']"
+61,"are there any papers dealing with acoustic wave propagation in reacting
+gases .","['565', '566', '564', '1159', '661']"
+62,"has anyone investigated relaxation effects on gaseous heat transfer to a
+suddenly heated wall .","['566', '567', '1084', '1078', '1081']"
+66,are there any theoretical methods for predicting base pressure .,"['664', '629', '180', '659', '660']"
+67,does transition in the hypersonic wake depend on body geometry and size,"['2', '3', '664', '629', '323', '324', '393', '128', '180', '394', '659', '389', '4', '1302']"
+68,how can one detect transition phenomena in boundary layers .,"['662', '101', '460', '661', '62']"
+69,how can one detect transition phenomena in hypersonic wakes .,"['458', '570', '977', '62', '336']"
+71,"has anyone investigated and developed a simple model for the vortex
+wake behind a cruciform wing .","['569', '571', '1355', '101', '655', '1213', '798', '572']"
+72,"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 .","['21', '324', '630', '94', '664', '304', '128', '323', '663', '570', '494', '305', '309', '571', '655', '388', '62']"
+74,"can the transonic flow around an arbitrary smooth thin airfoil be
+analysed in a simple approximate way .","['576', '656', '575', '317', '574', '578']"
+79,"what are the details of the rigorous kinetic theory of gases .
+(chapman-enskog theory) .","['597', '598', '688', '708', '713']"
+80,"has anyone investigated the effect of surface mass transfer on
+hypersonic viscous interactions .","['594', '597', '596', '598']"
+81,"what is the combined effect of surface heat and mass transfer on
+hypersonic flow .","['672', '799']"
+82,"what are the existing solutions for hypersonic viscous interactions over
+an insulated flat plate .","['676', '677', '678', '679', '205']"
+83,what controls leading-edge attachment at transonic speeds .,"['680', '681', '682', '683']"
+84,"can the three-point boundary-value problem for the blasius equation
+be integrated numerically,  using suitable transformations,  without
+iteration on the boundary conditions .","['606', '406', '608', '142', '294', '354', '522', '962', '1192', '1213', '873']"
+85,"what are the effects of small amounts of gas rarefaction on the
+characteristics of the boundary layers on slender bodies of revolution .","['608', '406', '606', '710']"
+86,"what is the available information pertaining to boundary layers on very
+slender bodies of revolution in continuum flow (the ?transverse
+curvature  effect) .","['594', '790']"
+87,"what is the available information pertaining to the effect of slight
+rarefaction on boundary layer flows (the ?slip? effect) .","['606', '611', '562', '50', '236', '609', '612', '406']"
+93,"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 .",['691']
+94,"how is the heat transfer downstream of the mass transfer region effected
+by mass transfer at the nose of a blunted cone .","['24', '283', '294', '559', '689', '690', '101', '1393', '354', '1104', '1161', '1395']"
+95,"to what extent can the available information for incompressible boundary
+layers be applied to problems involving compressible boundary layers .","['283', '662']"
+97,"to what extent can readily available steady-state aerodynamic data be
+utilized to predict lifting-surface flutter characteristics .","['699', '700', '701', '698', '1289', '702', '703', '779', '1339', '681']"
+98,"what are the significant steady and non-steady flow characteristics
+which affect the flutter mechanism .","['713', '708', '709', '711', '712']"
+99,"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) .","['717', '719', '1001', '1379']"
+100,"how much is known about boundary layer flows along non-circular
+cylinders .","['821', '822', '824', '820', '823', '825', '1122', '1051', '1121']"
+101,"is there any simple,  but practical,  method for numerical integration
+of the mixing problem (i.e. the blasius problem with three-point
+boundary conditions) .","['817', '818', '819', '820', '825', '824']"
+102,"does there exist a closed-form expression for the local heat transfer
+around a yawed cylinder .","['728', '913', '910', '911']"
+103,"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 .","['826', '828']"
+104,where can i find pressure data on surfaces of swept cylinders .,"['833', '834', '835', '836', '837']"
+105,"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 .","['848', '844', '845', '846', '847']"
+106,"does the boundary layer on a flat plate in a shear flow induce a
+pressure gradient .","['847', '846', '849', '844', '845']"
+107,"can the procedure of matching inner and outer solutions for a viscous
+flow problem be applied when the main stream is a shear flow .","['725', '728', '729', '911', '720', '75', '909']"
+108,"can series expansions be found for the boundary layer on a flat plate in
+a shear flow .","['724', '726', '727', '75', '909', '720', '723']"
+109,"what possible techniques are available for computing the injection
+distribution corresponding to an isothermal transpiration cooled
+hemisphere .","['860', '861', '606', '980', '12']"
+110,"what is known regarding asymptotic solutions to the exact boundary layer
+equations .","['862', '863', '31', '1174']"
+111,previous solutions to the boundary layer similarity equations .,"['15', '391', '864', '914', '392', '627', '658']"
+112,experimental results on hypersonic viscous interaction .,"['731', '730']"
+113,"what has been done about viscous interactions in relatively low reynolds
+number flows,  particularly at high mach numbers .","['746', '748', '749', '265']"
+114,"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 .","['919', '916', '920', '921']"
+116,"how significant is the possible pressure of a dissociated free stream
+with respect to the realization of hypersonic simulation in high
+enthalpy wind tunnels .","['922', '360', '605', '927', '492']"
+118,"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 .","['923', '924', '925']"
+119,"how far can one trust the linear viscosity-temperature solution
+assumed in some of the analyses of hypersonic shock layer at low
+reynolds number .",['926']
+120,"how close is the comparison of the shock layer theory with existing
+experiments in the low reynolds number (merged-layer) regime .","['829', '887', '890', '885', '886', '888', '889', '1146', '891']"
+121,"has anyone explained the kink in the surge line of a multi-stage
+axial compressor .","['885', '886', '1146', '887', '888', '890', '891']"
+122,"have any aerodynamic derivatives been measured at hypersonic mach
+numbers and comparison been made with theoretical work .","['931', '932', '934', '935', '936', '937', '938', '957', '1131']"
+123,"are methods of measuring aerodynamic derivatives available which
+could be adopted for use in short running time facilities .","['966', '967']"
+126,"what are wind-tunnel corrections for a two-dimensional aerofoil
+mounted off-centre in a tunnel .","['974', '1326', '187', '969', '970', '971', '972', '973']"
+128,"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 .","['985', '990']"
+130,what is the present state of the theory of quasi-conical flows .,"['766', '858', '859', '1008', '12']"
+131,"references on the methods available for accurately estimating
+aerodynamic heat transfer to conical bodies for both laminar and turbulent
+flow .","['1014', '1020', '1013', '1016', '1017', '1012', '1018', '1019']"
+132,"what parameters can seriously influence natural transition
+from laminar to turbulent flow on a model in a wind tunnel .","['1014', '1013', '1015', '1016', '1012', '1018', '1019', '1017', '951', '1023', '1020', '952', '1024', '1025', '1026']"
+133,"can a satisfactory experimental technique be developed for measuring
+oscillatory derivatives on slender sting-mounted models in supersonic
+wind tunnels .","['1020', '1018', '1019', '1024', '1012', '1016', '1022']"
+135,"what effect has the boundary layer in modifying the basic inviscid flow
+behind the shock,  neglecting effects of leading edge and corner .","['1018', '1017', '1023', '1024', '1025', '1026', '950', '1016']"
+136,"how does a satellite orbit contract under the action of air drag in
+an atmosphere in which the scale height varies with altitude .","['1021', '1022', '1034']"
+137,"how is the flow at transonic speeds about a delta wing different
+from that on a closely-related tapered sweptback wing .","['1029', '1034', '951', '1021']"
+138,recent data on shock-induced boundary-layer separation .,"['846', '1036']"
+139,what interference effects are likely at transonic speeds .,"['1031', '1032', '1035', '1037']"
+140,"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 .","['1038', '1039', '1041', '1042', '1043', '1044']"
+141,"can methane-air combustion product be used as a hypersonic test
+medium and predict, within experimental accuracies, the results
+obtained in air .","['1038', '1041', '1043', '1044', '1039', '1042']"
+142,"what is the theoretical heat transfer rate at the stagnation point of a
+blunt body .",['1042']
+143,what is the theoretical heat transfer distribution around a hemisphere .,"['1043', '1044']"
+145,"has anyone investigated the unsteady lift distributions on finite
+wings in subsonic flow .","['763', '838', '839', '1045', '743', '852', '841']"
+146,"what information is available for dynamic response of airplanes to
+gusts  or blasts in the subsonic regime .","['840', '1045']"
+147,"will forward or apex located controls be effective at low subsonic
+speeds and how do they compare with conventional trailing-edge
+flaps .","['889', '1046', '1048', '1047', '1049', '1051', '1050', '843', '926', '822']"
+148,"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 .","['889', '1048', '1050', '1046', '1049', '843']"
+149,"what are the effects of initial imperfections on the elastic buckling of
+cylindrical shells under axial compression .","['1057', '1058', '1059', '1052', '930', '931', '934', '936', '937', '938', '1131']"
+150,"why does the incremental theory and the deformation theory of plastic
+stress-strain relationship differ greatly when applied to stability
+problems .","['1074', '1075']"
+152,basic dynamic characteristics of structures continuous over many spans .,"['1076', '1077', '569', '572', '687', '655']"
+153,is the information on the buckling of sandwich sphere available .,"['1078', '1083', '1084', '1080', '1081', '1082', '1085']"
+154,"can the load deformation characteristics of a beam be obtained with the
+material being inelastic and a non uniform temperature being present .","['1087', '1088']"
+155,"what is the effect of an internal liquid column on the breathing
+vibrations of a cylindrical shell .","['1103', '1100', '983', '1101', '1104', '1099']"
+156,experimental techniques in shell vibration .,"['983', '1102', '1097', '1100', '274', '1096', '1098', '1099', '1103', '982', '1104', '553', '1101', '82']"
+157,"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 .","['273', '1105', '1106', '93', '161', '302', '122', '666', '1107', '556', '25', '1011', '19', '35', '1355', '372', '410', '456', '36', '44', '215', '626', '1151', '354', '369', '370', '421', '557', '605', '655', '657', '689', '1307', '318', '423', '1304', '160', '482', '572']"
+158,what data is there on the fatigue of structures under acoustic loading .,"['302', '1011', '552', '998', '1009', '1010', '273', '556']"
+160,panels subjected to aerodynamic heating .,"['1134', '1137', '1138', '1135', '1136']"
+161,"can increasing the edge loading of a plate beyond the critical value for
+buckling change the buckling mode .","['54', '1386', '562', '336', '55', '996']"
+163,"have the effects of an elastic edge restraint been considered in
+previous papers on panel flutter .","['20', '56', '57']"
+164,"has the solution of the clamped plate problem,  in the classical theory
+of bending,  been reduced to two successive membrane boundary value
+problems .","['311', '415', '416', '798', '316', '335', '1364', '1367']"
+165,"what data exists on oscillatory aerodynamic forces on control surfaces
+at transonic mach numbers .","['71', '72']"
+167,"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 .","['274', '82']"
+168,"is the problem of similarity for representative investigations of
+aeroelastic effects in heated flow as intractable as previous investigations
+imply .","['217', '774']"
+169,"what is the magnitude and distribution of lift over the cone and the
+cylindrical portion of a cone-cylinder configuration .","['118', '157', '774', '775']"
+170,"is there any information on how the addition of a /boat-tail/ affects
+the normal force on the body of various angles of incidence .","['139', '238', '239', '904', '906', '672']"
+171,"what are the aerodynamic interference effects on the fin lift and body
+lift of a fin-body combination .","['252', '431', '141']"
+173,"what is the effect of initial axisymmetric deviations from circularity
+on the non linear (large-deflection) load-deflection response of
+cylinders under hydrostatic pressure .","['367', '451']"
+175,"are previous analyses of circumferential thermal buckling of circular
+cylindrical shells unnecessarily involved or even inaccurate due to the
+assumed forms of buckling mode .","['351', '966', '967', '964', '965']"
+176,"what papers are there dealing with circumferential buckling either
+thermal buckling or due to mechanical loading .","['582', '583', '584', '585', '978', '586', '982']"
+177,"what analytical investigations have been made of the stability of
+conical shells . how do the results compare with experiment .","['588', '589', '592', '772', '590']"
+181,"has any work been done on determining the nature of compressible
+viscous flow in a straight channel .","['973', '974', '409', '997', '1061']"
+182,"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 .","['685', '686']"
+183,jet interference with supersonic flow  -dash experimental papers .,"['803', '808', '802', '807', '811', '253', '804', '805', '806', '809', '810', '1243', '1247']"
+184,thrust vector control by fluid injection -dash papers .,"['32', '67', '715', '717', '716', '499', '1379']"
+187,"is it possible to obtain a reasonably simple analytical solution to the
+heat equation for an exponential (in time) heat input .","['838', '839', '840', '743', '842', '1045']"
+189,"has anyone programmed a pump design method for a high-speed digital
+computer .","['395', '866', '869', '865', '868', '870', '867', '872', '873']"
+190,"has anyone derived simplified pump design equation from the fundamental
+three-dimensional equations for incompressible nonviscous flow .","['15', '391', '285', '390', '864']"
+196,"what are the flutter characteristics of the exposed skin panels of the
+x-15 vertical stabilizer when subjected to aerodynamic heating .","['51', '185', '874', '878', '879', '880', '12', '875', '876', '202', '746', '13']"
+200,"what agreement is found between theoretically predicted instability
+times and experimentally measured collapse times for compressed columns
+in creep .","['1134', '1137', '1138']"
+201,theoretical studies of creep buckling .,"['552', '625', '1296', '93', '1151', '401', '110', '1391', '423', '541', '1295', '318', '1304', '160', '369', '482']"
+202,experimental studies of creep buckling .,"['1303', '1304', '1309', '1306', '1308', '605', '602', '603', '604', '1110', '1305', '1310', '48', '232']"
+203,"is it possible to correlate the results on the creep buckling of widely
+different structures within the framework of a single theory .","['58', '1305', '1306', '602', '603', '604', '1307', '1310', '19', '232', '323', '688', '122', '1188']"
+204,what are the experimental results for the creep buckling of columns .,"['572', '1311', '63', '540', '602', '603', '604', '1305', '1188', '307', '1213', '655', '1355', '68']"
+205,"what are the results for the creep buckling of round tubes under
+external pressure .","['1321', '1322']"
+206,"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 .","['1338', '1341', '1340']"
+208,"has the effect of initial stresses,  on the frequencies of vibration of
+circular cylindrical shells,  been investigated .","['163', '1344', '1345', '164', '1347', '1346']"
+209,"has the effect of the change of initial pressure due to deformation,  on
+the frequencies of vibration of circular cylindrical shells been
+investigated .","['1351', '1356', '1350', '187', '487', '45', '55', '316', '1383', '1385', '1106', '1228']"
+210,"what are the discontinuity stresses at junctions in pressurized
+structures .","['1171', '891', '1172', '1173', '1030', '1174']"
+211,"what analytical solutions are available for stresses in edge-loaded
+shells of revolution .","['891', '1172', '1173', '1174', '763', '769', '1030', '1031', '1033', '1052', '1068']"
+212,"what dome contours minimize discontinuity stresses when used as closures
+on cylindrical pressure vessels .","['888', '889', '1178', '885', '887', '886', '841', '1176', '1177', '890', '769', '891', '1173', '843']"
+213,"what general solutions for the stresses in pressurized shells of
+revolution are available .","['888', '885', '887', '889', '1178', '769', '1173', '1177', '886', '890', '843']"
+214,"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 .","['833', '1361', '1362', '1363']"
+215,"what are the best experimental data and classical small deflection
+theory analyses available for pressurized cylinders in bending .","['37', '35']"
+216,"does a membrane theory exist by which the behaviour of pressurized
+membrane cylinders in bending can be predicted .",['156']
+217,"what are the equations which define the stability of simply supported
+corrugated core sandwich cylinders .","['666', '667', '1258', '1394', '668', '670', '1204', '1391', '1395', '1300', '37', '559', '630', '1107', '1213']"
+218,papers on small deflection theory for buckling of sandwich cylinders .,"['24', '101', '666', '667', '93', '1258', '1393', '559', '630', '662', '1104', '1107', '1204', '1213', '1300']"
+219,"has anyone developed an analysis which accurately establishes the large
+deflection behaviour of conical shells .","['1391', '666', '667', '1258', '1078', '1080', '1081', '1394', '1395', '1214', '1198', '1204', '1300', '559', '630', '662', '1107', '1213']"
+223,"what is the magnitude of second-order wing-body interference
+at high supersonic mach number .","['400', '1387', '1392', '1398']"
+224,"what is the best theoretical method for calculating pressure on the
+surface of a wing alone .","['656', '1313', '1317', '1316', '1318', '1319', '1157', '1274']"
+225,"how can the effect of the boundary-layer on wing pressure be calculated,
+and what is its magnitude .","['1379', '1305', '1304', '40', '293', '1309', '161', '421', '1377', '1378', '1381', '225', '1380', '448', '449', '1124', '1280', '433', '923', '924', '1062', '1074', '1075', '1213']"
+226,how should the navier-stokes difference equations be solved .,[]
+227,"which  iterative method for solving linear elliptic
+difference equations is most rapidly convergent .",[]
+230,technical report on measurement of ablation during flight .,[]
+231,"what qualitative and quantitative material is available on ablation
+materials research .",[]
+232,"have flow fields been calculated for blunt-nosed bodies and compared
+with experiment for a wide range of free stream conditions and body
+shapes .",[]
+233,what are the available properties of high-temperature air .,[]
+234,"what is the magnitude of aerodynamic damping in flexible vibration modes
+of a slender body of revolution characteristic of launch vehicles .",[]
+241,"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 .",[]
+245,"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 .",[]
+246,"what accurate or exact solutions of the laminar separation point for
+various incompressible and compressible boundary layers with zero heat
+transfer are available .",[]
+247,"can the hypersonic similarity results be applied to the technique of
+predicting surface pressures of an ogive forebody at angle of attack .",[]
+250,what determines the onset of shock-induced boundary-layer separation .,[]
+251,"are the stable profiles of a compressible boundary layer induced by a
+moving wave known .",[]
+252,"are there experimental results on the stability of a compressible
+boundary layer induced by a moving wave .",[]
+253,"exact solution methods for calculating the ablative mass loss of a
+material ablating at high temperatures in a hypersonic flight
+environment .",[]
+254,"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 .",[]
+255,"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 .",[]
+257,"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 .",[]
+259,"has a comparison been made between interference-free drag measurements
+using free-flight models and similar measurements made in a low-blockage
+wind tunnel .",[]
+261,solution of the blasius problem with three-point boundary conditions .,[]
+264,"references on lyapunov's method on the stability of linear
+differential equations with periodic coefficients .",[]
+265,"obtain all papers and reports that contain shock detachment distance
+data .",[]
+266,work on flow in channels at low reynolds numbers .,[]
+267,"some approximate analytical heat conduction solutions using methods
+other than biot's principle .",[]
+268,"what mode of stalling can be expected for each stage of an axial
+compressor .",[]
+269,"has a criterion been established for determining the axial compressor
+choking line .",[]
+272,"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 .",[]
+273,how does scale height vary with altitude in an atmosphere .,[]
+274,"jet interference with supersonic flows
+theoretical papers .",[]
+275,"effects of leading-edge bluntness on the flutter characteristics of some
+square-planform double-wedge airfoils at mach numbers less than 15.4.",[]
+277,"what factors have been shown to have a primary influence on sonic boom
+strength .",[]
+283,work on small-oscillation re-entry motions .,[]
+284,experimental studies on panel flutter .,[]
+285,"how can wing-body,  flow field interference effects be approximated
+rationally .",[]
+288,"has anyone analytically or experimentally investigated the effects of
+internal pressure on the buckling of circular-cylindrical shells under
+bending .",[]
+291,"what theoretical and experimental work has been done on the excitation
+and response of typical structures in a noise environment .",[]
+292,"is there a design method for calculating thermal fatigue endurances of
+components of various types and sizes in a variety of circumstances .",[]
+293,"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 .",[]
+294,"what is the criterion for true panel flutter,  as opposed to small
+amplitude vibration arising from acoustic disturbances .",[]
+295,papers dealing with uniformly loaded sectors .,[]
+296,general methods of solving clamped plate problems .,[]
+297,"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 .",[]
+298,"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 .",[]
+299,"the problem of similarity for representative investigation of
+aeroelastic effects in a flow with the absence of heating effects .",[]
+300,how is fatigue damage estimated using the normal long-hand method .,[]
+301,"is there any information available on the difference in the effects of
+various edge conditions on the buckling of cylindrical shells .",[]
+303,"have non-linear large deflection analyses been conducted for shell
+shapes other than conical .",[]
+304,"are asymptotic methods sufficiently accurate in the determination of
+pre-buckling stresses in torispherical shells,  or must we resort to
+numerical methods .",[]
+306,"what are the nonequilibrium chemical constituents in the viscous shock
+layer ahead of a blunt re-entry vehicle .",[]
+314,"how accurate are existing analytical theories in estimating pressure
+distributions on cones at incidence,  at hypersonic speeds .",[]
+315,"are simple empirical methods of any use for estimating pressure
+distribution in cones .",[]
+316,do viscous effects seriously modify pressure distributions .,[]
+317,"has anyone investigated theoretically whether surface flexibility
+can stabilize a laminar boundary layer .",[]
+321,"how do subsonic and transonic flutter data measured in the new langley
+transonic dynamics tunnel compare with similar data obtained in other
+facilities .",[]
+323,"how do large changes in new mass ratio quantitatively affect
+wing-flutter boundaries .",[]
+327,"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 .",[]
+331,"what are the physical significance and characteristics of separated
+laminar and turbulent boundary layer flows .",[]
+332,"has anyone analytically investigated the stabilizing influence of soft
+elastic cores on the buckling strength of cylindrical shells subjected
+to non-uniform external pressure .",[]
+333,"what papers are available on the buckling of empty cylindrical shells
+under non-uniform pressure .",[]
+335,"what effect do thermal stresses have on the compressive buckling
+strength of ring-stiffened cylinders .",[]
+336,"what is the effect on cylinder buckling of a circumferential stress
+system that varies in the axial direction .",[]
+338,"can non-linear shallow shell analysis be reduced to an engineering
+technique by use of the matrix .",[]
+339,"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 .",[]
+340,"what investigations have been made of the wave system created by a
+static pressure distribution over a liquid surface .",[]
+347,"has anyone investigated the effect of shock generated vorticity on heat
+transfer to a blunt body .",[]
+348,what is the heat transfer to a blunt body in the absence of vorticity .,[]
+349,"what are the general effects on flow fields when the reynolds number is
+small .",[]
+352,"find a calculation procedure applicable to all incompressible laminar
+boundary layer flow problems having good accuracy and reasonable
+computation time .",[]
+353,"papers applicable to this problem (calculation procedures for laminar
+incompressible flow with arbitrary pressure gradient) .",[]
+355,has anyone investigated the shear buckling of stiffened plates .,[]
+356,papers on shear buckling of unstiffened rectangular plates under shear .,[]
+360,"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 .",[]
+365,"what design factors can be used to control lift-drag ratios at mach
+numbers above 5 .",[]