Kooperativer Bibliotheksverbund

UID:

Format: VIII, 190 S. : Ill. ; 25 cm

Note: Literaturverz. S. 169-180

Language: Undetermined

UID:

Format: II, 21 S. 4"

Series Statement: (National Advisory Committee for Aeronautics. Report 1038)

Language: Undetermined

UID:

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)

UID:

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

URL: Volltext  (Deutschlandweit zugänglich)

UID:

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

URL: Volltext  (Deutschlandweit zugänglich)