Kooperativer Bibliotheksverbund

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Format: 243 S.

Series Statement: Princeton aeronautical paperbacks 6

Language: English

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Format: III, 40 S. 4"

Series Statement: (National Advisory Committee for Aeronautics. Report 1050)

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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

URL: Volltext  (Deutschlandweit zugänglich)

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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 (433 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. 10678

Note: A graphical method of determining pressure distribution in two-dimensional flow, by Robert T. Jones and Doris Cohen, N.A.C.A. [No. 722], p. 313 , A high-speed motion-picture study of normal combustion, knock, and preignition in a spark-ignition engine, by A.M. Rothrock, R.C. Spencer, and Cearcy D. Miller, N.A.C.A. [No. 704], p. 15 , A simplified theoretical method of determining the characteristics of a lifting rotor in forward flight, by F.J. Bailey, Jr., N.A.C.A. [No. 716], p. 209 , An analysis of the stability of an airplane with free controls, by Robert T. Jones and Doris Cohen, N.A.C.A. [No. 709], p. 109 , An apparatus for measuring rates of discharge of a fuel-injection system, by Francis J. Dutee, N.A.C.A. [No. 714], p. 193 , Analysis and prediction of longitudinal stability of airplanes, by R.R. Gilruth and M.D. White, N.A.C.A. [No. 711], p. 137 , Appendix, p. 118 , Determination of control-surface characteristics from NACA plain-flap and tab data, by Milton B. Ames, Jr. and Richards I. Sears, N.A.C.A. [No. 721], p. 295 , Effect of aging on mechanical properties of aluminum-alloy rivets, by Frederick C. Roop, National Bureau of Standards [No. 724], p. 353 , Effect of body nose shape on the propulsive efficiency of a propeller, by G.W. Stickle, John L. Crigler, and Irven Naiman, N.A.C.A. [No. 725], p. 371 , Flow coefficients of monosleeve valves, by C.D. Waldron, N.A.C.A. [No. 717], p. 227 , Internal-flow systems for aircraft, by F.M. Rogallo, N.A.C.A. [No. 713], p. 165 , Lateral control required for satisfactory flying qualities based on flight tests of numerous airplanes, by R.R. Gilruth and W.N. Turner, N.A.C.A. [No. 715], p. 201 , Preignition characteristics of several fuels under simulated engine conditions, by R.C. Spencer, N.A.C.A. [No. 710], p. 121 , Pressure available for cooling with cowling flaps and tab data, by George W. Stickle, Irven Naiman, and John L. Crigler, N.A.C.A. [No. 720], p. 283 , Pressure distribution over an NACA 23021 airfoil with a slotted and a split flap, by Thomas A. Harris and John G. Lowry, N.A.C.A. [No. 718], p. 241 , Propeller analysis from experimental data, by George M. Stickle and John L. Crigler, N.A.C.A. [No. 712], p. 147 , Tests of the NACA 0025 and 0035 airfoils in the full-scale wind tunnel, by W. Kenneth Bullivant, N.A.C.A. [No. 708], p. 91 , The additional-mass effect of plates as determined by experiments, by William Gracey, N.A.C.A. [No. 707], p. 81 , The design of fins for air-cooled cylinders, by Arnold E. Biermann and Herman H. Ellerbrock, Jr. [No. 726], p. 401 , The problem of cooling an air-cooled cylinder on an aircraft engine, by M.J. Brevoort and U.T. Joyner, N.A.C.A. [No. 719], p. 267 , Wind-tunnel investigation of NACA 23012, 23021, and 23030 airfoils equipped with 40-percent-chord double-slotted flaps, by Thomas A. Harris and Isidore G. Recant, N.A.C.A. [No. 723], p. 321 , Wind-tunnel investigation of effect of interference on lateral-stability characteristics of four NACA 23012 wings, an elliptical and a circular fuselage, and vertical fins, by Rufus O. House and Arthur R. Wallace, N.A.C.A. [No. 705], p. 31 , Wind-tunnel investigation of spoiler deflector, and slot lateral-control devices on wings with full-span split and slotted flaps, by Carl J. Wenzinger and Francis M. Rogallo, N.A.C.A. [No. 706], p. 51 , © 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

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Format: 1 online resource (252 p.)

ISBN: 9781400874941

Series Statement: Princeton Aeronautical Paperbacks ; 2204

Content: Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes.Originally published in 1960.The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

Note: Frontmatter -- , Preface -- , Contents -- , A. Aerodynamics of Wings at High Speeds -- , Chapter 1. Fundamental Considerations in the Development of Wings for High Speeds -- , Chapter 2. Aerodynamics of Thin Wings at Subsonic Speeds -- , Chapter 3. Aerodynamics of Thin Wings at Supersonic Speeds , In English.

Language: English

DOI: 10.1515/9781400874941

URL: https://doi.org/10.1515/9781400874941

URL: https://www.degruyter.com/isbn/9781400874941