Kooperativer Bibliotheksverbund

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Format: Online-Ressource (1660 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 12096

Note: A second-order shock-expansion method applicable to bodies of revolution near zero lift, by Clarence A Syvertson and David H. Dennis, NACA [No. 1328], p. 1127 , A summary and analysis of the low-speed longitudinal characteristics of swept wings at high Reynolds numbers, by G. Chester Furlong and James G. McHugh, NACA [No. 1339], p. 1390 , A theoretical study of the aerodynamics of slender cruciform-wing arrangements and their wakes, by John R. Spreiter and Alvin H. Sacks, NACA [No. 1296], p. 81 , Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers, by Julian D. Maynard and Leland B. Salters, Jr., NACA [No. 1309], p. 651 , An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-wing airplane, by Richard B. Skoog, NACA [No. 1298], p. 125 , An evaluation of four experimental methods for measuring mean properties of supersonic turbulent boundary layer, by George J. Nothwang, NACA [No. 1320], p. 939 , An investigation of four wings of square plan form at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel, by Charles M. McLellan, Mitchel H. Bertram, and John A. Moore, NACA [No. 1310], p. 675 , An investigation of single- and duel-rotation propellers at positive and negative thrust, and in combination with an NACA 1-Series D-Type cowling at mach numbers up to 0.84, by Robert M. Reynolds, Robert I. Sammonds, and John H. Walker, NACA [No. 1336], p. 1269 , Attention in shock tube due to unsteady-boundary-layer action, by Harold Mirels, NACA [No. 1333], p. 1227 , Average properties of compressible laminar boundary layer on flat plate with unsteady flight velocity, by Franklin K. Moore and Simon Ostrach, NACA [No. 1325], p. 1037 , Basic considerations in the combustion of hydrocarbon fuels with air, by Propulsion Chemistry Division, Lewis Flight Propulsion Laboratory, NACA [No. 1300], p. 187 , Bodies of revolution having minimum drag at high supersonic airspeeds, by A.J. Eggers, Jr., Meyer M. Resnikoff, and David H. Dennis, NACA [No. 1306], p. 555 , Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7, by Rinaldo J. Brun, NACA [No. 1317], p. 785 , Comparison of several methods for obtaining the time response of linear systems to either a unit impulse or arbitrary input from frequency-response data, by James J. Donegan and Carl R. Huss, NACA [No. 1324], p. 1023 , Correlation, evaluation, and extension of linearized theories for tire motion and wheel shimmy, by Robert F. Smiley, NACA [No. 1299], p. 137 , Determination of longitudinal stability and control characteristics from free-flight model tests with results at transonic speeds for three airplane configurations, by Clarence L. Gillis and Jess L. Mitchell, NACA [No. 1337], p. 1327 , Determination of vortex paths by series expansion technique with application to cruciform wings, by Alberta Y. Alksne, NACA [No. 1311], p. 693 , Experimental and predicted longitudinal and lateral-directional response characteristics of a large flexible 35 [degree] swept-wing airplane at an altitude of 35,000 feet, by Henry A. Cole, Jr., Stuart C. Brown, and Euclid C. Holleman, NACA [No. 1330], p. 1165 , Exploratory investigation of boundary-layer transition on a hollow cylinder at a mach number of 6.9, by Mitchel H. Bertram, NACA [No. 1313], p. 723 , Far noise-field of air jets and jet engines, by Edmund E. Callaghan and Willard D. Coles, NACA [No. 1329], p. 1147 , Flight and analytical methods for determining the coupled vibration response of tandem helicopters, by John E. Yeates, Jr., George W. Brooks, and John C. Houbolt, NACA [No. 1326], p. 1049 , Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes, by William H. Phillips, Helmut A. Kuehnel and James B. Whitten, NACA [No. 1304], p. 505 , Induced velocities near a lifting rotor with nonuniform disk loading, by Harry H. Heyson and S. Katzoff, NACA [No. 1319], p. 850 , Influence of alloying upon grain-boundary creep, by F.N. Rhines, W.E. Bond, and M.A. Kissel, Carnegie Institute of Technology, [No. 1331], p. 1205 , Influence of hot-working conditions on high-temperature properties of a heat-resistant alloy, by John F. Ewing and J.W. Freeman, University of Michigan, [No. 1341], p. 1599 , Investigation of downwash, sidewash, and Mach number distribution behind a rectangular wing at a mach number of 2.41 by David Adamson and William B. Boatright, NACA [No. 1340], p. 1541 , Investigation of the compressive strength and creep lifetime of 2024-T3 aluminum-alloy plates at elevated temperatures, by Eldon E. Mathauser and William D. Deveikis, NACA [No. 1308], p. 637 , Investigation of the laminar aerodynamic heat-transfer characteristics of a hemisphere-cylinder in the Langley 11-inch hypersonic tunnel at Mach number 6.8, by Davis H. Crawford and William D. McCauley, NACA [No. 1323], p. 1001 , Lift and center of pressure of wing-body-tail combination at subsonic, transonic, and supersonic speeds, by William C. Pitts, Jack N. Nielsen, and George E. Kaatari, NACA [No. 1307], p. 567 , Linearized lifting-surface and lifting-line evaluations of sidewash behind rolling triangular wings a supersonic speeds, by Percy J. Bobitt, NACA [No. 1301], p. 455 , List of technical reports, p. III , Measurement of aerodynamic forces for various mean angles of attack on an airfoil oscillating in pitch and on two finite-span wings oscillating in bending with emphasis on damping in the stall, by A. Gerald Rainey, NACA [No. 1305], p. 520 , Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow, by Harry L. Runyan and Donald S. Woolston, NACA [No. 1321], p. 971 , Minimum wave drag for arbitrary arrangements of wings and bodies, by Robert T. Jones, NACA [No. 1335], p. 1263 , Near noise field of a jet-engine exhaust, by Walton L. Howes, Edmund E. Callaghan, Willard D. Coles, and Harold R. Mull, NACA [No. 1338], p. 1355 , Nonlifting wing-body combinations with certain geometric restraints having minimum wave drag at low subsonic speeds, by Harvard Lomax, NACA [No. 1297], p. 113 , On panel flutter and divergence of infinitely long unstiffened and ring-stiffened thin-walled circular cylinders, by Robert W. Leonard and John M. Hedgepeth, NACA [No. 1302], p. 475 , On slender-body theory at transonic speeds, by Keith C. Harder and E.B. Klunker, NACA [No. 1315], p. 765 , Relation of turbojet and ramjet combustion efficiency to second-order reaction kinetics and fundamental flame speed, by J. Howard Childs, Thaine W. Reynolds, and Charles C. Graves, NACA [No. 1334], p. 1249 , Seat design for crash worthiness, by I. Irving Pinkel and Edmund G. Rosenberg, NACA [No. 1332], p.1211 , Some effects on bluntness on boundary-layer transition and heat transfer at supersonic speeds, by W.E. Moeckel, NACA [No. 1312], p. 709 , Summary of scale-model thrust-reverser investigation, by John H. Povolny, Fred W. Steffen and Jack G. McArdle, NACA [No. 1314], p. 751 , Table of contents, p. II , Theoretical calculation for the power spectra of the rolling and yawing moments of a wing in random turbulence, by John M. Eggleston and Franklin W. Diederich, NACA [No. 1321], p. 951 , Three-dimensional transonic flow theory applied to slender wings and bodies, by Max A. Heaslet and John R. Spreiter, NACA [No. 1318], p. 820 , Torsional stiffness of thin-walled shells having reinforcing cores and rectangular, triangular, or diamond cross section, by Harvey G. McComb, Jr., NACA [No. 1316], p. 771 , Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack - subsonic, transonic, and supersonic speeds, by William Gracey, NACA [No. 1303], p. 495 , theoretical and experimental investigation of the subsonic-flow fields beneath swept and unswept wings with tables of vortex-induced velocities, by William J. Alford, Jr., NACA [No. 1327], p. 1083 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: Online-Ressource (1503 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 12180

Note: A comparative analysis of the performance of long-range hypervelocity vehicles, by Alfred J. Eggers, Jr., H. Julian Allen, and Stanford E. Neice, NACA [No. 1382], p. 1141 , A correlation of results of a flight investigation with results of an analytical study of effects of wing flexibility on wing strains due to gusts, by C.C. Shufflebarger, Chester B. Payne, and George L. Cahen, NACA [No. 1365], p. 669 , A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary layer transition, by Albert F. Von Doenhoff and Elmer A. Horton, NACA [No. 1349], p. 239 , A method for simulating the atmospheric entry of long-range ballistic missiles, by A.J. Eggers, Jr., NACA [No. 1378], p. 1009 , A method of computing the transient temperature of thick walls form arbitrary variation of adiabatic-wall temperature and heat-transfer coefficient, by P.R. Hill, NACA [No. 1372], p. 877 , A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures, by Elbridge Z. Stowell, NACA [No. 1343], p. 125 , A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver, by Leonard Sternfield, NACA [No. 1344], p. 131 , A study of the motion and aerodynamic heating of ballistic missiles entering the earth's atmosphere at hight supersonic speeds, by H. Julian Allen and A.J. Eggers, Jr. NACA [No. 1381], p. 1125 , A summary of preliminary investigations into the characteristics of combustion screech in ducted burners, by Lewis Laboratory Staff, NACA [No. 1384], p. 1195 , A theoretical and experimental study of planing surfaces including effects of cross section and plan form, by Charles L. Shuford, Jr., NACA [No. 1355], p. 373 , A variational theorem for creep with applications to plates and columns, by J. Lyell Sanders, Jr., Harvey G. McComb, Jr., and Floyd R. Schlechte, NACA [No. 1342], p. 117 , A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96, by Albert J. Evans and George Liner, NACA [No. 1375], p. 933 , An analysis of pressure studies and experimental and theoretical downwash and sidewash behind five pointed-tip wings at supersonic speeds, by William B. Boatright, NACA [No. 1380], p. 1067 , An experimental investigation of sting-support effects on drag and a comparison with jet effects at transonic speeds, by Maurice S. Cahn, NACA [No. 1353], p. 327 , Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses, by Richard R. Heldenfels and Louis F. Vosteen, NACA [No. 1361], p. 593 , Area-suction boundary-layer control as applied to the trailing-edge flaps of a 35 [degree] swept-wing airplane, by Woodrow L. Cook, Seth B. Anderson, and George E. Cooper, NACA [No. 1370], p. 823 , Blowing-type boundary-layer control as applied to the trailing-edge flaps of a 25 [degree] swept-wing airplane, by Mark W. Kelly, Seth B. Anderson, and Robert C. Innis, NACA [No. 1369], p. 799 , Boron and zirconium from crucible refractories in a complex heat-resistant alloy, by R.F. Decker, John P. Rowe, and J.W. Freeman, University of Michigan, [No. 1392], p. 1457 , Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine, by Leslie W. Lassiter and Robert W. Hess, NACA [No. 1367], p. 703 , Characteristics of the Langley 8-foot transonic tunnel with slotted test section, by Ray H. Wright, Virgil S. Ritchie, and Albin O. Pearson, NACA [No. 1389], p. 1297 , Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number, by Eli Reshotku and Ivan E. Beckwith, NACA [No. 1379], p. 1016 , Differential equations of motion for combined flapwise vending, chordwise bending, and torsion of twisted non-uniform rotor blades, by John C. Houbolt and George W. Brooks, NACA [No. 1346], p. 179 , Ditching investigations of dynamic models and effects of design parameters on ditching characteristics, by Lloyd J. Fisher and Edward L. Hoffman, NACA [No. 1347], p. 197 , Drag minimization for wings and bodies in supersonic flow, by Max A. Heaslet and Franklyn B. Fuller, NACA [No. 1385], p. 1213 , Effect of chord size on weight and cooling characteristics of air-cooled turbine blades, by Jack B. Esgar, Eugene F. Schum, and Arthur N. Curren, NACA [No. 1354], p. 359 , Effect of fuel variables on carbon formation in turbojet-engine combustors, by Edmund R. Jonash, Jerrold D. Wear, and William P. Cook, NACA [No. 1352], p. 309 , Elliptic cones alone and with wings at supersonic speeds, by Leland H. Jorgensen, NACA [No. 1376], p. 975 , Experimental determination of effects of frequency and amplitude on the lateral stability derivatives for a delta, a swept, and an unswept wing oscillating in yaw, by Lewis R. Fisher, NACA [No. 1357], p. 461 , Full-scale investigation of several jet-engine noise-reduction nozzles, by Willard D. Coles and Edmund E. Callaghan, NACA [No. 1387], p. 1249 , Ground simulator studies of the effects of valve friction, stick friction, flexibility, and backlash on power control system quality, by B. Porter Brown, NACA [No. 1348], p. 225 , Growth of disturbances in a flame-generated shear region, by Perry L. Blackshear, Jr., NACA [No. 1360], p. 546 , Incompressible flutter characteristics of representative aircraft wings, by C.H. Wilts, California Institute of Technology, [No. 1390], p. 1385 , Investigation of a nonlinear control system, by I. Flugge-Lotz, C.F. Taylor, and H.E. Lindberg, Stanford University, [No. 1391], p. 1423 , Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition, by Dean R. Chapman, Donald M. Kuehn, and Howard K. Larson, NACA [No. 1356], p. 419 , Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2, by Leland H. Jorgensen and Edward W. Perkins, NACA [No. 1371], p. 857 , Investigation of the drag of various axially symmetric nose shapes of fineness ratio 3 for Mach numbers from 1.24 to 7.4, by Edward W. Perkins, Leland H. Jorgensen, and Simon C. Sommer, NACA [No. 1386], p. 1231 , List of technical reports, p. III , Measurement of static pressure on aircraft, by William Gracey, NACA [No. 1364], p. 643 , Measurements of free-space oscillating pressures near propellers at flight Mach numbers to 0.72, by Max C. Kurbjun and Arthur W. Vogeley, NACA [No. 1377], p. 999 , Methods for obtaining desired helicopter stability characteristics and procedures for stability predictions, by F.B. Gustafson and Robert J. Topscott, NACA [No. 1350], p. 255 , NACA Research on slurry fuels, by M.L. Pinns, W.T. Olson, H.C. Barnett, and R. Breitwieser, NACA [No. 1388], p. 1273 , On flow of electrically conducting fluids over a flat plate in presence of a transverse magnetic field, by Vernon J. Rossow, NACA [No. 1358], p. 489 , Origin and prevention of crash fires in turbojet aircraft, by I. Irving Pinkel, Solomon Weiss, G. Merritt Preston, and Gerard J. Pesman, NACA [No. 1363], p. 623 , Survey of hydrogen combustion properties, by Isadore L. Drell and Frank E. Belles, NACA [No. 1383], p. 1161 , Systemic two-dimensional cascade tests of NACA 65-Series compressor blades at low speeds, by James C. Emery, L. Joseph Herrig, John R. Erwin, and A. Richard Felix, NACA [No. 1368], p. 713 , Table of contents, p. II , The mechanism of thermal-gradient mass transfer in the sodium hydroxide - nickel system, by Charles E. May, NACA [No. 1366], p. 683 , The response of an airplane to random atmospheric disturbances, by Franklin W. Diederich, NACA [No. 1345], p. 142 , The similarity rules for second-order subsonic and supersonic flow, by Milton D. Van Dyke, NACA [No. 1374], p. 925 , Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus- and liner cross-sectional areas, by Charles C. Graves and Jack S. Grobman, NACA [No. 1373], p. 899 , Theoretical combustion performance of several high-energy fuels for ramjet engines, by Leonard K. Tower, Roland Breitwieser, and Benson E. Gammon, NACA [No. 1362], p. 605 , Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades, by Robert P. Coleman and Arnold M. Feingold, NACA [No. 1351], p. 267 , Thin airfoil theory based on approximate solution of the transonic flow equation, by John R. Spreiter and Alberta Y. Alksne, NACA [No. 1359], p. 509 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: Online-Ressource (1386 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 11917

Note: A correlation by means of transonic similarity rules of experimentally determined characteristics of a series of symmetrical and cambered wings of rectangular plan form, by John B. McDevitt, NACA [No. 1253], p. 1355 , A flight evaluation of the longitudinal stability characteristics associated with the pitch-up of a swept-wing airplane in maneuvering flight at transonic speeds, by Seth B. Anderson and Richard S. Bray, NACA [No. 1237], p. 843 , A free-flight wind tunnel for aerodynamic testing at hypersonic speeds, by Alvin Seiff, NACA [No. 1222], p. 381 , A method for the design of swept-back wings warped to produce specified flight characteristics at supersonic speeds, by Warren A. Tucker, NACA [No. 1226], p. 459 , A theoretical and experimental investigation of the lift and drag characteristics of hydrofoils at subcritical and supercritical speeds, by Kenneth L. Wadlin, Charles L. Shuford, Jr., and John R. McGehee, NACA [No. 1232], p. 661 , A unified two-dimensional approach to the calculation of three-dimensional hypersonic flows, with application to bodies of revolution, by A.J. Eggers, Jr., and Raymond C. Savin, NACA [No. 1249], p. 1189 , An experimental study of applied ground loads in landing, by Benjamin Milwitzky, Dean C. Lindquist, and Dexter M. Potter, NACA [No. 1248], p. 1155 , An investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61, by K.R. Czarnecki and Archibald R. Sinclair, NACA [No. 1240], p. 929 , An investigation of the maximum lift of wings at supersonic speeds, by James J. Gallagher and James N. Mueller, NACA [No. 1227], p. 477 , Analog study of interacting and non-interacting multiple-loop control systems for turbojet engines, by George J. Pack and W.E. Philips, Jr., NACA [No. 1212], p. 97 , Analysis and calculation by integral methods of laminar compressible boundary layer with heat transfer and with and without pressure gradient, by Morris Morduchow, Polytechnic Institute of Brooklyn, [No. 1245], p. 1065 , Analysis of turbulent heat transfer, mass transfer, and friction in smooth tubes at high Prandtl and Schmidt numbers, by Robert G. Diessler, NACA [No. 1210], p. 69 , Arrangement of fusiform bodies to reduce the wave drag at supersonic speeds, by Morris D. Friedman and Doris Cohen, NACA [No. 1236], p. 835 , Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow, by Franklin W. Diederich and Martin Zlotnick, NACA [No. 1228], p. 505 , Calculation of laminar heat transfer around cylinders of arbitrary cross section and transpiration-cooled walls with application to turbine blade cooling, by E.R.G. Eckert and J.N.B. Livingood, NACA [No. 1220], p. 339 , Characteristics of turbulence in a boundary layer with zero pressure gradient, by P.S. Klebanoff, National Bureau of Standards, [No. 1247], p. 1135 , Charts for estimating tail-rotor contribution to helicopter directional stability and control in low-speed flight, by Kenneth B. Amer and Alfred Gessow, NACA [No. 1216], p. 185 , Determination of lateral -stability derivatives and transfer-function coefficients from frequency-response data for lateral motions, by James J. Donegan, Samuel W. Robinson, Jr., and Ordway B. Gates, Jr., NACA [No. 1225], p. 439 , Effect of ground interference on aerodynamic and flow characteristics of a 42 [degree] sweptback wing Reynolds numbers up to 6.8X10(6), by G. Chester Furlong and Thomas V. Bollech, NACA [No. 1218], p. 251 , Effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of a delta-wing model, by Alex Goodman and David F. Thomas, NACA [No. 1224], p. 407 , Error in airspeed measurement due to the static-pressure field ahead of an airplane at transonic speeds, by Thomas C. O'Bryan, Edward C.B. Danforth, and J. Ford Johnston, NACA [No. 1239], p. 915 , Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperature, by Patrick L. Donoughe and John N.B. Livingood, NACA [No. 1229], p. 573 , Experimental investigation of free-convection heat transfer in vertical tube at large Grashof numbers, by E.R.G. Eckert and A.J. Diaguila, NACA [No. 1211], p. 83 , Free-stream boundaries of turbulent flows, by Stanley Corrsin and Alan L. Kistler, The Johns Hopkins University, [No. 1244], p. 1033 , Generalized indicial forces on deforming rectangular wings in supersonic flight, by Harvard Lomax, Franklyn B. Fuller, and Loma Sluder, NACA [No. 1230], p. 595 , High-resolution autoradiography, by George C. Towe, Henry J. Gomberg, and J.W. Freeman, University of Michigan, [No. 1243], p. 979 , Impingement of cloud droplets on a cylinder and procedure for measuring liquid-water content and droplet sized in supercooled clouds by rotating multicylinder method, by R.J. Brun, W. Lewis, P.J. Perkins, and J.S. Serafini, NACA [No. 1215], p. 139 , Investigation at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles, by Eugene S. Love, NACA [No. 1238], p. 855 , List of technical reports, p. III , Measurement and analysis of wing and tail buffeting loads on fighter airplane, by Wilber B. Huston and T.H. Skopinski, NACA [No. 1219], p. 311 , Minimum-drag ducted and pointed bodies of revolution based on linearized supersonic theory, by Hermon M. Parker, NACA [No. 1213], p. 111 , NACA transonic wind-tunnel test sections, by Ray H. Wright and Vernon G. Ward,NACA [No. 1231], p. 623 , On the kernel function of the integral equation relating the lift of downwash distributions of oscillating finite wings in subsonic flow, by Charles E. Watkins, Harry L. Runyan, and Donald S. Woolston, NACA [No. 1234], p. 703 , Quasi-cylindrical theory of wing-body interference at supersonic speeds and comparison with experiment, by Jack N. Nielsen, NACA [No. 1252], p. 1299 , Shock-turbulence interaction and the generation of noise, by H.S. Ribner, NACA [No. 1233], p. 682a , Standard atmosphere - tables and data for altitudes to 65,800 feet, by International Aviation Organization and NACA, [No. 1235], p. 719 , Statistical measurements on contact conditions of 478 transport-airplane landings during routine daytime operations, by Norman S. Silsby, NACA [No. 1214], p. 121 , Stress-analysis of circular semimonocoque cylinders with cutouts, by Harvey G. McComb, NACA [No. 1251], p. 1243 , Table of contents, p. II , The dynamic-response characteristics of a 35 [degree] swept-wing airplane as determined from flight measurements, by William C. Triplett, Stuart C. Brown, and G. Allan Smith, NACA [No. 1250], p. 1217 , The hydrodynamic characteristics of modified rectangular flate plates having aspect rations of 1.00, 0.25, and 0.125 and operating near a free water surface, by Kenneth L. Wadlin, John A. Ramsen, and Victor L. Vaughan, Jr., NACA [No. 1246], p. 1085 , Theoretical and analog studies of the effects of nonlinear stability derivatives on the longitudinal motions of an aircraft in response to step control deflections and to the influence of proportional automatic control, by Howard J. Curfman, Jr., NACA [No. 1241], p. 941 , Theoretical and experimental investigation of heat transfer by laminar natural convection between parallel plates, by A.F. Lietzke, NACA [No. 1223], p. 399 , Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds, by John R. Spreiter and Alverta Alksne, NACA [No. 1217], p. 207 , Theoretical study of the tunnel-boundary lift interference due to slotted walls in the presence of the trailing -vortex system of the lifting model, by Clarence W. Matthews, NACA [No. 1221], p. 361 , Transonic flow past cone cylinders, by George E. Solomon, California Institute of Technology, [No. 1222], p. 963 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

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Format: Online-Ressource (1452 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 11595

Note: A comparison of theory and experiment for high-speed free-molecule flow, by Jackson R. Stalder, Glen Goodwin, and Marcus O. Creager [No. 1032], p. 735 , A general integral form of the boundary-layer equation for incompressible flow with an application to the calculation of the separation point of turbulent boundary layers, by Neal Tetervin and Chia Chiao Lin [No. 1046], p. 1067 , A lift-cancellation technique in linearized supersonic-wing theory, by Harold Mirels [No. 1004], p. 65 , A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions, by Richard R. Heldenfels [No. 1043], p. 1019 , A recurrence matrix solution for the dynamic response of aircraft in gusts, by John C. Houbolt [No. 1010], p. 145 , A small-deflection theory for curved sandwich plates, by Manuel Stein and J. Mayers [No. 1008], p. 129 , A study of effects of viscosity on flow over slender inclined bodies of revolution, by H. Julian Allen and Edward W. Perkins [No. 1048.], p. 1103 , A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results, by John D. Bird and Byron M. Jaquet [No. 1031], p. 709 , A summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow, by Arthur L. Jones and Alberta Alksne [No. 1052], p. 1211 , A theoretical analysis of the effect of time lag in an automatic stabilization system on the lateral oscillatory stability of an airplane, by Leonard Sternfield and Ordway B. Gates, Jr. [No. 1018], p. 291 , An analysis of base pressure at supersonic velocities and comparison with experiment, by Dean R. Chapman [No. 1051], p. 1187 , Analysis of means of improving the uncontrolled lateral motions of personal airplanes, by Marion O. McKinney, Jr. [No. 1035], p. 795 , Analysis of plane-plastic-stress problems with axial symmetry in strain-hardening range, by M.H. Lee Wu [No. 1021], p. 359 , Analysis of the effects of boundary-layer control on the take-off and power-off landing performance characteristics of a liaison type of airplane, by Elmer A. Horton, Laurence K. Loftin, Jr., Stanley F. Racisz, and John H. Quinn, Jr. [No. 1057], p. 1353 , Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection, by E. Clinton Wilcox and Arthur M. Trout [No. 1006], p. 97 , Analysis of turbulent free-convection boundary layer on flat plate, by E.R.G. Eckert and Thomas W. Jackson [No. 1015], p. 255 , Analytical determination of coupled bending-torsion vibrations of cantilever beams by means of station functions, by Alexander Mendelson and Selwyn Gendler [No. 1005], p. 77 , Buckling of thin-walled cylinder under axial compression and internal pressure, by Hsu Lo, Harold Crate, and Edward B. Schwartz [No. 1027], p. 647 , Calculation of the lateral control of swept and unswept flexible wings of arbitrary stiffness, by Franklin W. Diederich [No. 1024], p. 413 , Comparison between theory and experiment for wings at supersonic speeds, by Walter G. Vincenti [No. 1033], p. 757 , Comparison of theoretical and experimental heat-transfer characteristics of bodies of revolution at supersonic speeds, by Richard Scherrer [No. 1055], p. 1301 , Compressive strength of flanges, by Elbridge Z. Stowell [No. 1029], p. 675 , Correlation of physical properties with molecular structure for some dicyclic hydrocarbons having high thermal-energy release per unit volume, by P.H. Wise, K.T. Serijan, and I.A. Goodman [No. 1003], p. 55 , Diffusion of chromium in alpha cobalt-chromium solid solutions, by John W. Weeton [No. 1023], p. 397 , Dynamics of a turbojet engine considered as a quasi-static system, by Edward W. Otto and Burt L. Taylor, III [No. 1011], p. 177 , Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow, by Charles E. Watkins [No. 1028], p. 657 , Effect of tunnel configuration and testing technique on cascade performance, by John R. Erwin and James C. Emery [No. 1016], p. 263 , Effects of wing flexibility and variable air lift wing bending moments during landing impacts of a small seaplane, by Kenneth F. Merten and Edgar B. Beck [No. 1013], p. 221 , Equations and charts for the rapid estimation of hinge-moment and effectiveness parameters for trailing-edge controls having leading and trailing edges swept ahead of the mach lines, by Kennith L. Goin [No. 1041], p. 937 , Experimental and theoretical studies of area suction for the control of the laminar boundary layer on an NACA 64A010 airfoil, by Albert L. Braslow, Dale L. Burrows, Neal Tetervin, and Fioravante Visconti [No. 1025], p. 433 , Experimental investigation of the effect of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics of a model with 45 [degree] sweptback wing and tail surfaces, by M.J. Queijo and Walter D. Wolhart [No. 1049], p. 1117 , Experimental investigation of the effects of viscosity on the drag and base pressure of bodies of revolution at a mach number of 1.5, by Dean R. Chapman and Edward W. Perkins [No. 1036], p. 805 , Formulas for the supersonic loading, lift, and drag of flat swept-back wings with leading edges behind the mach lines, by Doris Cohen [No. 1050], p. 1146 , General method and thermodynamic tables for computation of equilibrium composition and temperature of chemical reactions, by Vearl N. Huff, Sanford Gordon, and Virginia E. Morrell [No. 1037], p. 829 , Horizontal tail loads in maneuvering flight, by Henry A. Pearson, William A. McGowan, and James J. Donegan [No. 1007], p. 117 , Influence of chemical composition on rupture properties at 1200 [degrees] F. of forged chromium-cobalt-nickel-iron base alloys in solution-treated and aged condition, by E.E. Reynolds, J.W. Freeman, and A.E. White [No. 1058], p. 1385 , Integrals and integral equations in linearized wing theory, by Harvard Lomax, Max A. Heaslet, and Franklyn B. Fuller [No. 1054], p. 1267 , Investigation of frequency-response characteristics of engine speed for a typical turbine-propeller engine, by Burt L. Taylor, III, and Frank L. Oppenheimer [No. 1017], p. 279 , Investigation of fretting by microscopic observation, by Douglas Godfrey [No. 1009], p. 135 , Investigation of separation of the turbulent boundary layer, by G.B. Schubauer and P.S. Klebanoff, National Bureau of Standards [No. 1030], p. 689 , Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65 series wings equipped with full-span slotted flaps, by Jack Fischel and James M. Watson [No. 1034], p. 769 , Investigation of the NACA 4-(5)(08)-03 and NACA 4-(10)(08)-03 two-blade propellers at forward mach numbers to 0.725 to determine the effects of camber and compressibility on performance, by James B. Delano [No. 1012], p. 189 , Investigation of turbulent flow in a two-dimensional channel, by John Laufer, California Institute of Technology [No. 1053], p. 1247 , Measurements of average heat-transfer and friction coefficients for subsonic flow of air in smooth tubes at high surface and fluid temperatures, by Leroy V. Humble, Warren H. Lowdermilk, and Leland G. Desmon [No. 1020], p. 343 , NACA investigation of fuel performance in piston-type engines, by Henry C. Barnett [No. 1026], p. 453 , On the particular integrals of the Prandtl-Busemann iteration equations for the flow of a compressible fluid, by Carl Kaplan [No. 1039], p. 909 , Relation between inflammables and ignition sources in aircraft environments, by Wilfred E. Scull [No. 1019], p. 303 , Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane, by Leonard Sternfield [No. 1042], p. 1009 , Spectra and diffusion in a round turbulent jet, by Stanley Corrsin and Mahinder S. Uberoi, Johns Hopkins University [No. 1040], p. 915 , Study of effects of sweep on the flutter of cantilever wings, by J.G. Barmby, H.J. Cunningham, and I.E. Garrick [No. 1014], p. 229 , Supersonic flow around circular cones at angles of attack, by Antonio Ferri [No. 1045], p. 1055 , Table of contents, p. II , Temperature distribution in internally heated walls of heat exchangers composed of non-circular flow passages, by E.R.G. Eckert and George M. Low [No. 1022], p. 381 , The method of characteristics for the determination of supersonic flow over bodies of revolution at small angles of attack, by Antonio Ferri [No. 1044], p. 1039 , The stability of the compression cover of box beams stiffened by posts, by Paul Seide and Paul F. Barrett [No. 1047], p. 1087 , Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds, by John DeYoung [No. 1056], p. 1317 , Wind-tunnel investigation of air inlet and outlet openings on a streamline body, by John V. Becker [No. 1038], p. 887 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

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Series Statement: (National Advisory Committee for Aeronautics. Report 1052)

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