Kooperativer Bibliotheksverbund

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Format: II, VI S. 4"

Series Statement: (National Advisory Committee for Aeronautics. Report 1039)

Language: Undetermined

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Format: Online-Ressource (634 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 10018

Note: A comparison of fuel sprays from several types of injection nozzles, by Dana W. Lee [No. 520], p. 251 , A flight investigation of the spinning of the F4B-2 biplane with various loads and tail surfaces, by N.F. Scudder and Oscar Seidman [No. 529], p. 413 , A turbulence indicator utilizing the diffusion of heat, by G.B. Schubauer [No. 524], p. 337 , Aerodynamic characteristics of a wing with fowler flaps, including flap loads downwash, and calculated effect of take-off, by Robert C. Platt [No. 534], p. 477 , Aerodynamic characteristics of wings with cambered external-airfoil flaps, including lateral control with a full-span flap, by Robert C. Platt [No. 541], p. 609 , Air flow in a separating laminar boundary layer, by G.B. Schubauer [No. 527], p. 369 , Altitude-pressure tables based on the United States Standard Atmosphere, by W.G. Brombacher [No. 538], p. 531 , An analysis of longitudinal stability in power-off flight with charts for use in design, by Charles H. Zimmerman [No. 521], p. 289 , Analysis of 2-spar cantilever wings with special reference to torsion and load transference, by Paul Kuhn [No. 508], p. 45 , Appendices, p. 64 , Appendix, p. 201 , Appendix, p. 249 , Appendix, p. 318 , Appendix, p. 487 , Appendix, p. 76 , Characteristics of the N.A.C.A. 23012 airfoil from tests in the full-scale and variable-density tunnels, by Eastman N. Jacobs and William C. Clay [No. 530], p. 435 , Distribution and regularity of injection from a multicylinder fuel-injection pump, by A.M. Rothrock and E.T. Marsh [No. 533], p. 465 , Experimental investigation of the Robinson-type cup anemometer, by M.J. Brevoort and U.T. Joyner [No. 513], p. 143 , Flight investigation of lateral control devices for use with full-span flaps, by H.A. Soule and W.H. McAvoy [No. 517], p. 209 , Full-scale wind-tunnel tests of a PCA-2 autogiro rotor, by John B. Wheatley and Manley J. Hood [No. 515], p. 179 , General equations for the stress analysis of rings, by Eugene E. Lundquist and Walter F. Burke [No. 509], p. 69 , Hydrogen as an auxiliary fuel in compression-ignition engines, by Harold C. Gerrish and Hampton H. Foster [No. 535], p. 495 , Interference of wing and fuselage from tests of 209 combinations in the N.A.C.A. variable-density tunnel, by Eastman N. Jacobs and Kenneth E. Ward [No. 540], p. 571 , Investigation of full-scale split trailing-edge wing flaps with various chords and hinge locations, by Rudolf Wallace [No. 539], p. 545 , List of technical reports, p. III , Noise from two-blade propellers, by E.Z. Stowell and A.F. Deming [No. 526], p. 359 , Potential flow about elongated bodies of revolution, by Carl Kaplan [516], p. 189 , Reduction of hinge moments of airplane control surfaces by tabs, by Thomas A. Harris [No. 528], p. 381 , Some effects of injection advance angle, engine-jacket temperature, and speed on combustion in a compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 525], p. 343 , Some factors affecting combustion in an internal-combustion engine, by A.M. Rothrock and Mildred Cohn [No. 512], p. 125 , Spinning characteristics of wings. I. -- Rectangular Clark Y monoplane wing, by M.J. Bamber and C.H. Zimmerman [No. 519], p. 231 , Tests in a variable-density wind tunnel of related airfoils having the maximum camber unusually far forward, by Eastman N. Jacobs and Robert M. Pinkerton [No. 537], p. 521 , The drag of airplane wheels, wheel fairings and landing gears. II. -- Nonretractable and partly retractable landing gears, by David Biermann and William H. Herrnstein, Jr. [No. 518], p. 219 , The drag of airplane wheels, wheel fairings, and landing gears -- III, by William H. Herrnstein, Jr. and David Biermann [No. 522], p. 321 , The effect of baffles on the temperature distribution and heat-transfer coefficients of finned cylinders, by Oscar W. Schey and Vern G. Rollin [No. 511], p. 111 , The effect of water vapor on flame velocity in equivalent CO-O2 mixtures, by Ernest F. Fiock and H. Kendall King [No. 531], p. 445 , The influence of wing setting on the wing lead and rotor speed of a PCA-2 autogiro as determined in flight, by John B. Wheatley [No. 323], p. 333 , The measurements of the field of view from airplane cockpits, by Melvin N. Gough [No. 514], p. 167 , The soap-bubble method of studying the combustion of mixtures of CO and O2, by Ernest F. Fiock and Carl H. Roeder [No. 532], p. 451 , Wind-tunnel research comparing lateral control devices particularly at high angles of attack. XIII. -- Auxiliary airfoils used as external ailerons, by Fred E. Weick and Richard W. Noyes [No. 510], p. 79 , Wind-tunnel tests of a 10-foot-diameter gyroplane rotor, by John B. Wheatley and Carlton Bioletti [No. 536], p. 511 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: Online-Ressource (1199 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. 11676

Note: A biharmonic relaxation method for calculating thermal stress in cooled irregular cylinders, by Arthur G. Holms [No. 1059], p. 71 , A study of second-order supersonic flow theory, by Milton D. Van Dyke [No. 1081], p. 489 , A theoretical analysis of the effects of fuel motion on airplane dynamics, by Albert A. Sehy [No. 1080], p. 467 , Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow, by Charles E. Watkins and Julian H. Berman [No. 1099], p. 863 , Airfoil profiles for minimum pressure drag at supersonic velocities -- general analysis with application to linearized supersonic flow, by Dean R. Chapman [No. 1063], p. 129 , An empirically derived basis for calculating the area, rate, and distribution of water-drop impingement on airfoils, by Norman R. Bergrun [No. 1107], p. 1079 , An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer, by Arthur Earl Bryson, Jr. [No. 1094], p. 725 , An iterative transformation procedure for numerical solution of flutter and similar characteristic-value problems, by Myron L. Gossard [No. 1073], p. 303 , Analysis of temperature distribution in liquid-cooled turbine blades, by John N.B. Livingood and W. Byron Brown [No. 1066], p. 169 , Analysis of the effects of wing interference on the tail contributions to the rolling derivatives, by William H. Michael, Jr. [No. 1086], p. 569 , Automatic control systems satisfying certain general criterions on transient behavior, by Aaron S. Boksenbom and Richard Hood [No. 1068], p. 207 , Axisymmetric supersonic flow in rotating impellers, by Arthur W. Goldstein [No. 1083], p. 523 , Chordwise and compressibility corrections to slender-wing theory, by Harvard Lomax and Loma Sluder [No. 1105], p. 1049 , Comparison of high-speed operating characteristics of size 215 cylindrical-roller bearings as determined in turbojet engine and in laboratory test rig, by E. Fred Macks and Zolton N. Nemeth [No. 1084], p. 537 , Correlation of physical properties with molecular structure for some dicyclic hydrocarbons having high thermal-energy release per unit volume -- 2-alkylbiphenyl and the two isomeric 2-alkylbicyclohexyl series, by Irving A. Goodman and Paul H. Wise [No. 1065], p. 159 , Detailed computational procedure for design of cascade blades with prescribed velocity distributions in compressible potential flows, by George R. Costello, Robert L. Cummings, and John T. Sinnette, Jr. [No. 1060], p. 91 , Discussion of boundary-layer characteristics near the wall of an axial-flow compressor, by Artur Mager, John J. Mahoney, and Ray E. Budinger [No. 1085], p. 549 , Effect of aspect ratio on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with flap and with retractable ailerons, by Jack Fischel, Rodger L. Naeseth, John R. Hagerman, and William M. O'Hare [No. 1091], p. 649 , Effect of initial mixture temperature on flame speed of methane-air, propane-air and ethylene-air mixtures, by Gordon L. Dugger [No. 1061], p. 105 , Effects of compressibility on the performance of two full-scale helicopter rotors, by Paul J. Carpenter [No. 1078], p. 449 , Effects on longitudinal stability and control characteristics of a Boeing B-29 airplane of variations in stick-force and control-rate characteristics obtained through use of a booster in the elevator-control system, by Charles W. Mathews, Donald B. Talmadge, and James B. Whitten [No. 1076], p. 375 , Experimental aerodynamic derivatives of a sinusoidally oscillating airfoil in two-dimensional flow, by Robert L. Halfman [No. 1108], p. 1101 , Experimental determination of the effect of horizontal tail size, tail length, and vertical location on low-speed static longitudinal stability and damping in pitch of a model having 45 [degree] sweptback wing and tail surfaces, by Jacob H. Lichtenstein [No. 1096], p. 789 , Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities, by Dean R. Chapman, William R. Wimbrow, and Robert H. Kester [No. 1109], p. 1145 , Flight investigation a mechanical feel device in an irreversible elevator control system of a large airplane, by B. Porter Brown, Robert G. Chilton, and James B. Whitten [No. 1101], p. 919 , Flight investigation of the effect of control centering springs on the apparent spiral stability of a personal-owner airplane, by John P. Campbell, Paul A. Hunter, Donald E. Hewes, and James B. Whitten [No. 1092], p. 697 , Generalization of boundary-layer momentum-integral equations to three-dimensional flows including those of rotating system, by Artur Mager [No. 1067], p. 191 , Generalized theory for seaplane impact, by Benjamin Milwitzky [No. 1103], p. 951 , Heat transfer to bodies in a high-speed rarified gas stream, by Jackson R. Stalder, Glen Goodwin and Marcus O. Creager [No. 1093] , Hydrodynamic impact of a system with a single elastic mode. I-- Theory and generalized solution with an application to an elastic airframe, by Wilbur L. Mayo [No. 1074], p. 349 , Hydrodynamic impact of a system with a single elastic mode. II - Comparison of experimental force and response with theory, by Robert W. Miller and Kenneth F. Merton [No. 1075], p. 367 , Inelastic column behavior, by John E. Duberg and Thomas W. Wilder, III [No. 1072], p. 286 , Internal-liquid-film-cooling experiments with airstream temperatures to 2000 [degrees] F in 2- and 4- inch diameter horizontal tubes, by George R. Kinney, Andrew E. Abramson and John L. Sloop [No. 1087], p. 581 , Investigation of wear and friction properties under sliding conditions of some materials suitable for cages of rolling-contact bearings, by Robert L. Johnson, Max A. Swikert, and Edmond E. Bisson [No. 1062], p. 117 , List of technical reports, p. III , Lubrication and cooling studies of cylindrical-roller bearings at high speeds, by E. Fred Macks and Zolton N. Nemeth [No. 1064], p. 143 , Matrix method of determining the longitudinal-stability coefficients and frequency response of an aircraft from transient flight data, by James J. Donegan and Henry A. Pearson [No. 1070], p. 233 , Method for calculating lift distributions for unswept wings with flaps or ailerons by use of nonlinear section lift data, by James C. Sivell and Gertrude C. Westrick [No. 1090], p. 623 , Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design, by Joseph T. Hamrick, Ambrose Ginsburg, and Walter M. Osborn [No. 1082], p. 513 , On a solution of the nonlinear differential equation for transonic flow past a wave-shaped wall, by Carl Kaplan [No. 1069], p. 221 , On reflection of shock waves from boundary layers, by H.W. Liepmann, A. Roshko and S. Dhawan [No. 1100], p. 889 , Preliminary investigation of a new type of supersonic inlet, by Antonio Ferri and Louis M. Nucci [No. 1104], p. 1029 , Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment, by Harry L. Runyan [No. 1089], p. 615 , Some features of artificially thickened fully developed turbulent boundary layers with zero pressure gradient, by P.S. Klebanoff and Z.W. Diehl [No. 1110], p. 1165 , Sound from a two-blade propeller at supersonic tip speeds, by Harvey H, Hubbard and Leslie W. Lassiter [No. 1079], p. 457 , Stresses in a two-bay noncircular cylinder under transverse loads, by George E. Griffith [No. 1097], p. 811 , Summary of methods for calculating dynamic lateral stability and response and for estimating lateral stability derivatives, by John P. Campbell and Marion O. McKinney [No. 1098], p. 823 , Table of contents, p. II , The Langley annular transonic tunnel, by Louis W. Habel, James H. Henderson, and Mason F. Miller [No. 1106], p. 1069 , The linearized charateristics method and its application to practical nonlinear supersonic problems, by Antonio Ferri [No. 1102], p. 933 , Theoretical damping in roll and rolling moment due to differential wing incidence for slender cruciform wings and wing-body combinations, by Gaynor J. Adams and Duane W. Dugan [No. 1088], p. 603 , Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan forum at subsonic speeds, by John DeYoung [No. 1071], p. 245 , Transonic flow past a wedge profile with detached bow wave, by Walter G. Vincenti and Cleo B. Wagoner [No. 1095], p. 759 , Two- and three-dimensional unsteady lift problems in high-speed flight, by Harvard Lomax, Max A. Heaslet, Franklin B. Fuller and Loma Sluder [No. 1077], p. 393 , p. 715 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

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Format: Online-Ressource (1238 p) , illustrations, maps, 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. 11762

Note: A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory, by Clarence W. Matthews [No. 1155], p. 1125 , A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by the use of accelerometer and attitude-angle measurements, by John A. Zaloveik, Lindsay J. Lina, and James P. Trant, Jr. [No. 1145], p. 899 , A special investigation to develop a general method for three-dimensional photoelastic stress analysis, by M.M. Frocht and R. Guernsey, Jr. [No. 1148], p. 963 , A study of elastic and plastic stress concentration factors due to notches and fillets in flat plates, by Herbert F. Hardrath and Lachlan Ohman [No. 1117], p. 213 , A study of inviscid flow about airfoils at high supersonic speeds, by A.J. Eggers, Jr., Clarence A. Syvertson, and Samuel Kraus [No. 1123], p. 339 , A thermodynamic study of the turbine-propeller engine, by Benjamin Pinkel and Irving M. Karp [No. 1114], p. 117 , A vector study of linearized supersonic flow applications to nonplanar problems, by John C. Martin [No. 1143], p. 845 , Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes, by John M. Riebe and Rodger L. Naeseth [No. 1144], p. 879 , Aerodynamic forces and loadings on symmetrical circular-arc airfoils with plain leading-edge and plain trailing-edge flaps, by Jones F. Cahill, William J. Underwood, Robert J. Nuber, and Gail A. Cheesman [No. 1146], p. 913 , An analysis of laminar free-convection flow and heat transfer about a flat plate parallel to the direction of the generating body force, by Simon Ostrach [No. 1111], p. 63 , Analysis of landing-gear behavior, by Benjamin Milwitzky and Francis E. Cook [No. 1154], p. 1077 , Analytical derivation and experimental evaluation of short-bearing approximation for full journal bearings, by George B. DuBois and Fred W. Ocvirk [No. 1157], p. 1199 , Appendices, p. 72 , Application of a channel design method to high-solidity cascades and tests of an impulse cascade with 90 [degree] of turning, by John D. Stanitz and Leonard J. Sheldrake [No. 1116], p. 193 , Calculations on the forces and moments for an oscillating wing-aileron combination in two-dimensional potential flow at sonic speed, by Herbert C. Nelson and Julian H. Berman [No. 1128], p. 469 , Charts and approximate formulas for the estimation of aeroelastic effects on the lateral control of swept and unswept wings, by Kenneth A. Foss and Franklin W. Diederich [No. 1139], p. 715 , Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings, by Franklin W. Diederich and Kenneth A. Foss [No. 1140], p. 743 , Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow, by Harry L. Runyan and Charles E. Watkins [No. 1150], p. 993 , Deflection and stress analysis of thin solid wings of arbitrary plan form with particular reference to delta wings, by Manuel Stein, J. Edward Anderson, and John M. Hedgepeth [No. 1131], p. 513 , Design of two-dimensional channels with prescribed velocity distributions along the channel walls, by John D. Stanitz [No. 1115], p. 153 , Diffusion of heat from a line source in isotropic turbulence, by Mahinder S. Uberoi and Stanley Corrsin [No. 1142}, p. 815 , Direct measurements of skin friction, by Satish Dhawan [No. 1121], p. 281 , Displacement effect of a three-dimensional boundary layer, by Franklin K. Moore [No. 1124], p. 367 , Dynamics of mechanical feedback-type hydraulic servomotors under inertia loads, by Harold Gold, Edward W. Otto, and Victor L. Ransom [No. 1125], p. 373 , Equations, tables, and charts for compressible flow, by Ames Research staff [No. 1135], p. 611 , Estimation of the maximum angle of sideslip for determination of vertical-tail loads in rolling maneuvers, by Ralph W. Stone, Jr. [No. 1136], p. 683 , Experiments to determine neighborhood reactions to light airplanes with and without external noise reduction, by Fred S. Elwell [No. 1156], p. 1155 , Hydrocarbon and nonhydrocarbon derivatives of cyclopropane, by Vernon A. Slabey, Paul H. Wise, and Louis C. Gibbons [No. 1112], p. 81 , Initial results of instrument-flying trials conducted in a single-rotor helicopter, by Almer D. Crim, John P. Reeder, and James B. Whitten [No. 1137], p. 695 , Laminar boundary layer on cone in supersonic flow at large angle of attack, by Franklin K. Moore [No. 1132], p. 533 , List of technical reports, p. III , Mechanism of start and development of aircraft crash fires, by I. Irving Pinkel, G. Merritt Preston and Gerard J. Pesman [No. 1133], p. 546 , Method and graphs for the evaluation of air-induction systems, by George B. Brajinikoff [No. 1141], p. 793 , Method for calculation of laminar heat transfer in air flow around cylinders of arbitrary cross section (including large temperature differences and transpirational cooling), by E.R.G. Eckert and John N.B. Livingood [No. 1118], p. 223 , On the application of transonic similarity rules to wings of finite span, by John R. Spreiter [No. 1153], p. 1055 , On transonic flow past a wave-shaped wall, by Carl Kaplan [No. 1149], p. 981 , One-dimensional analysis of choked-flow turbines, by Robert E. English and Richard H. Cavicchi [No. 1127], p. 451 , Photographic investigation of combustion in a two-dimensional transparent rocket engine, by Donald R. Bellman, Jack C. Humphrey and Theodore Male [No. 1134], p. 599 , Reciprocity relations in aerodynamics, by Max A. Heaslet and John R. Spreiter [No. 1119], p. 253 , Relative importance of various sources of defect-producing hydrogen introduced into steel during application of vitreous coatings, by Dwight G. Moore, Mary A. Mason, and William N. Harrison [No. 1120], p. 269 , Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw, by John D. Bird, Lewis R. Fisher, and Sadie M. Hubbard [No. 1130], p. 495 , Spectrum of turbulence in a contracting stream, by H.S. Ribner and M. Tucker [No. 1113], p. 99 , Study of inadvertent speed increases in transport operation, by Henry A. Pearson [No. 1138], p. 703 , Survey of portions of the chromium-cobalt-nickel- molybdenum quaternary system at 1200 [degrees] C., by Sheldon Paul Rideout and Paul A. Beck [No. 1122], p. 301 , Table of contents, p. II , The effect of blade-section thickness ratios on the aerodynamic characteristics of related full-scale propellers at mach numbers up to 0.65, by Julian D. Maynard and Seymour Steinberg [No. 1126], p. 395 , The effects on dynamic lateral stability and control of large artificial variations in the rotary stability derivatives, by Robert O. Schade and James L. Hassell, Jr. [No. 1151], p. 1001 , The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight, by Frank M. Hamaker, Stanford E. Neice, and Thomas J. Wong [No. 1147], p. 951 , Theory and procedure for determining loads and motions in chine-immersed hydrodynamic impacts of prismatic bodies, by Emanuel Schnitzer [No. 1152], p. 1025 , Transverse vibrations of hollow thin-walled cylindrical beams, by Bernard Budiansky and Edwin T. Kruszewski [No. 1129], p. 485 , © 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

URL: Volltext  (Deutschlandweit zugänglich)

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Format: Online-Ressource (643 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 10318

Note: A discussion of certain problems connected with the design of hulls of flying boats and the use of general test data, by Walter S. Diehl [No. 625], p. 253 , A flight comparison of conventional ailerons on a rectangular wind and of conventional and floating wing-tip ailerons on a tapered wing, by H.A. Soule and W. Gracey [No. 630], p. 351 , A photographic study of combustion and knock in a spark-ignition engine, by A.M. Rothrock and R.C. Spencer [No. 622], p. 213 , A study of the torque equilibrium of an auto-giro rotor, by F.J. Bailey, Jr. [No. 623], p. 235 , Aerodynamic characteristics of a large number of airfoils tested in the variable-density wind tunnel, by Robert M. Pinkerton and Harry Greenberg [No. 628], p. 297 , Airfoil section characteristics as applied to the prediction of air forces and their distribution on wings, by Eastman N. Jacobs and R.V. Rhode [No. 631], p. 357 , Appendix, p. 130 , Approximate stress analysis of multistringer beams with shear deformation of the flanges, by Paul Kuhn [No. 636], p. 469 , Auto-ignition and combustion of diesel fuel in a constant-volume bomb, by Robert F. Selden [No. 617], p. 147 , Calculation of the chordwise load distribution over airfoil sections with plain, split, or serially hinged trailing-edge flaps, by H. Julian Allen [No. 634], p. 435 , Column strength of tubes elastically restrained against rotation at the ends, by William R. Osgood [No. 615], p. 101 , Comparative flight and full-scale wind-tunnel measurements of the maximum life of an airplane, by Abe Silverstein, S. Katzoff, and James A. Hootman [No. 618], p. 161 , Compressible flow about symmetrical Jonkowski profiles, by Carl Kaplan [No. 621], p. 197 , Determination of the boundary-layer transition on three symmetrical airfoils in the N.A.C.A. full-scale wind tunnel, by Abe Silverstein, and John V. Becker [No. 637], p. 491 , Drag of cylinders of simple shapes, by W.F. Lindsey [No. 619], p. 169 , Heat-transfer processes in air-cooled engine cylinders, by Benjamin Pinkel [No. 612], p. 49 , Interrelation of exhaust-gas constituents, by Harold C. Gerrish and Fred Voss [No. 616], p. 139 , List of technical reports, p. III , On sonic reciprocal relations in the theory of nonstationary flows, by I.E. Garrick [No. 629], p. 347 , Pressure distribution over airfoils with Fowler flaps, by Carl J. Wenzinger and Walter B. Anderson [No. 620], p. 177 , Pressure distribution over an N.A.C.A. 23012 airfoil with an N.A.C.A. 23012 external-airfoil flap, by Carl J. Wenzinger [No. 614], p. 85 , Pressure distribution over an N.A.C.A. 23012 airfoil with a slotted and a plain flap, by Carl J. Wenzinger and James B. Delano [No. 633], p. 403 , Tests of five full-scale propellers in the presence of a radical and a liquid-cooled engine nacelle, including test of two spinners, by David Biermann and Edwin P. Hartman [No. 642], p. 587 , The aerodynamic characteristics of four full-scale propellers having different plan forms, by Edwin P. Hartman and David Biermann [No. 643], p. 617 , The aerodynamic characteristics of full-scale propellers having 2, 3, and 4 blades of Clark Y and R.A.F 6 airfoil sections, by Edwin P. Hartman and David Biermann [No. 640], p. 547 , The crinkling strength and the bending strength of round aircraft tubing, by William R. Osgood [No. 632], p. 387 , The effect of compressibility on eight full-scale propellers operating in the take-off and climbing range, by David Biermann and Edwin P. Hartman [No. 639], p. 517 , The experimental and calculated characteristics of 22 tapered wings, by Raymond F. Anderson [No. 627], p. 273 , The influence of lateral stability on disturbed motions of an airplane with special reference to the motions produced by gusts, by Robert T. Jones [No. 638], p. 507 , The negative thrust and torque of several full-scale propellers and their application to various flight problems, by Edwin P. Hartman and David Biermann [No. 641], p. 571 , The torsional and bending deflection of full-scale aluminum-alloy propeller blades under normal operating conditions, by Edwin P. Hartman and David Biermann [No. 644], p. 627 , The transition phase in the take-off of an airplane, by J.W. Wetmore [No. 626], p. 261 , The variation with Reynolds number of pressure distribution over an airfoil section, by Robert M. Pinkerton [No. 613], p. 65 , Theoretical stability and control characteristics of wings with various amounts of taper and twist, by Henry A. Pearson and Robert T. Jones [No. 635], p. 451 , Two dimensional subsonic compressible flow past elliptical cylinders, by Carl Kaplan [No. 624], p. 245 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

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Format: Online-Ressource (432 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. 10825

Note: A study by high-speed photography of combustion and knock in a spark-ignition engine, by Cearcy D. Miller [No. 727], p. 15 , An investigation of the drag of windshields in 8-foot high-speed wind-tunnel, by Russell G. Robinson and James B. Delano [No. 730], p. 65 , Bending of rectangular plates with large deflections, by Samuel Levy [No. 737], p. 139 , Critical compressive stress for flat rectangular plates supported along all edges and elastically restrained against rotation along the unloaded edges, by Eugene E. Lundquist and Elbridge Z. Stowell [No. 733], p. 99 , Critical compressive stress for outstanding flanges, by Eugene E. Lundquist and Elbridge Z. Stowell [No. 734], p. 111 , Determination of optimum plan forms for control surfaces, by Robert T. Jones and Doris Cohen [No. 731], p. 79 , Drag and propulsive characteristics of air-cooled engine-nacelle installations for large airplanes, by Abe Silverstein and Herbert A. Wilson, Jr. [No. 746], p. 301 , Flutter calculations in three degrees of freedom, by Theodore Theodorsen and I.E. Garrick [No. 741], p. 223 , Ground effect on downwash angles and wake location, by S. Katzoff and Harold H. Sweberg [No. 738], p. 159 , High-speed tests of a model twin-engine low-wing transport airplane, by John V. Becker and Lloyd H. Leonard [No. 750], p. 391 , High-speed tests of conventional radial-engine cowlings, by Russell G. Robinson and John V. Becker [No. 745], p. 287 , Investigation in the 7-by 10-foot wind-tunnel of ducts for cooling radiators within an airplane wing, by Thomas A. Harris and Isidore G. Recant [No. 743], p. 249 , List of technical reports, p. III , Non-stationary flow about a wing-aileron tab combination including aerodynamic balance, by Theodore Theodorsen and I.E. Garrick [No. 736], p. 129 , Normal pressure tests of circular plates with clamped edges, by Albert E. McPherson, Walter Ramberg, and Samuel Levy [No. 744], p. 269 , Normal-pressure tests of rectangular plates, by Walter Ramberg, Albert E. McPherson, and Samuel Levy [No. 748], p. 349 , On the use of residue theory for treating the subsonic flow of a compressible fluid, by Carl Kaplan [No. 728], p. 39 , Pressure distribution over an NACA 23012 airfoil with a fixed slot and a slotted flap, by Thomas A. Harris and John G. Lowry [No. 732], p. 85 , Propeller charts for the determination of the rotational speed for the maximum ration of the propulsive efficiency to the specific fuel consumption, by David Biermann and Robert N. Conway [No. 749], p. 373 , Restraint provided a flat rectangular plate by a study stiffener along an edge of the plate, by Eugene E. Lundquist and Elbridge Z. Stowell [No. 735], p. 123 , Shear lag in box beams: Methods of analysis and experimental investigations, by Paul Kuhn and Patrick T. Chiarito [No. 739], p. 171 , Square plate with clamped edges under normal pressure producing large deflections, by Samuel Levy [No. 740], p. 209 , Test of a single-stage axial flow-fan, by E. Barton Bell [No. 729], p. 49 , The mean aerodynamic chord and the aerodynamic center of a tapered wing, by Walter S. Diehl [No. 751], p. 413 , Wind-tunnel investigation of an NACA 23012 airfoil with 30-percent-chord venetian-blind flaps, by F.M. Rogallo and Bartholomew S. Spano [No. 742], p. 241 , Wind-tunnel tests of four- and six-blade single- and dual-rotating tractor propellers, by David Biermann and Edwin P. Hartman [No. 747], p. 319 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

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Format: 1 online resource (17 pages, 1 unnumbered page) : , illustration.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 554

Note: "February 1936." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (14 pages, 1 unnumbered page) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; no. 762

Note: "May 1940." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (14 pages, 1 unnumbered page) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; no. 762

Note: "May 1940." , No Federal Depository Library Program (FDLP) item number.

Language: English