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Format: X, 620 S. mit Abb. 4"

Series Statement: (NASA SP-55)

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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

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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 (757 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. 10471

Note: A study of air flow in an engine cylinder, by Dana W. Lee [No. 653], p. 227 , A theoretical study of the moment on a body in a compressible fluid, by Karl Caplan [No. 671], p. 581 , Air flow in the boundary layer of an elliptic cylinder, by G.B. Schubauer [No. 652], p. 207 , Aircraft rate-of-climb indicators, by Daniel P. Johnson [No. 666], p. 473 , Airfoil section data obtained in the N.A.C.A. variable-density tunnel as affected by support interference and other corrections, by Eastman N. Jacobs and Ira H. Abbott [No. 669], p. 507 , Appendix, p. 69 , Calculation of the aerodynamic characteristics of tapered wings with partial-span flaps, by Henry A. Pearson and Raymond F. Anderson [No. 665], p. 455 , Cooling on the front of an air-cooled engine cylinder in a conventional engine cowling, by M.J. Brevoort and U.T. Joyner [No. 674], p. 625 , Correction of temperatures of air-cooled engine cylinders for variation in engine and cooling conditions, by Oscar W. Schey, Benjamin Pinkel, and Herman H. Ellerbrock, Jr. [No. 645], p. 49 , Design charts for predicting downwash angles and wake characteristics behind plain and flapped wings, by Abe Silverstein and S. Katzoff [No. 648], p. 107 , Design of N.A.C.A. cowlings for radial air-cooled engines, by George W. Stickle [No. 662], p. 383 , Determination of the profile drag of an airplane wing in flight at high Reynolds numbers, by Joseph Bicknell [No. 667], p. 483 , Downwash and wake behind plain and flapped airfoils, by Abe Silverstein, S. Katzoff, and W. Kenneth Bullivant [No. 651], p. 179 , Effect of service stresses on impact resistance, x-ray diffraction patterns and microstructure of 258 aluminum alloy, by J.A. Keyes and G.W. Quick [No. 659], p. 343 , Effects of elevator nose shape, gap, balance, and tabs, on the aerodynamic characteristics of a horizontal tail surface, by Harry J. Goett and J.P. Reeder [No. 675], p. 639 , Experimental investigation of the momentum method for determining profile drag, by Harry J. Goett [No. 660], p. 643 , Experimental verification of the theory of oscillating airfoils, by Abe Silverstein and Upshur T. Joyner [No. 673], p. 619 , Freen-spinning wind-tunnel tests in a low-wing monoplane with systematic changes in wings and tails -- IV. Effect of center-of-gravity location, by Oscar Seidman and A.I. Niehouse [No. 672], p. 599 , General airplane performance, by W.C. Rockefeller [No. 654], p. 241 , Interference with tail surface and wing and fuselage from tests of 17 combinations in the N.A.C.A. variable-density tunnel, by Albert Sherman [No. 678], p. 689 , List of technical reports, p. III , Surface heat-transfer coefficients of finned cylinders, by Herman H. Ellerbrock, Jr. and Arnold E. Biermann [No. 676], p. 651 , Tensile elastic properties of 18:8 chromium-nickel steel as affected by plastic deformation, by D.J. McAdam, Jr. and R.W. Mebs [No. 670], p. 539 , Tests in the variable-density wind tunnel of the N.A.C.A. 23012 airfoil with plain and split flaps, by Ira H. Abbott and Harry Greenberg [No. 661], p. 373 , Tests of N.A.C.A. 0009, 0012, and 0018 airfoils in the full-scale tunnel, by Harry J. Goett and W. Kenneth Bullivant [No. 647], p. 97 , Tests of two full-scale propellers with different pitch distributions, at blade angles up to 60 degrees, by David Biermann and Edwin P. Hartman [No. 658], p. 327 , The "pack" method for compressive tests of thin specimens of materials used in thin-wall structures, by C.S. Aitchison and L.B. Tuckerman [No. 649], p. 133 , The aerodynamic characteristics of six full-scale propellers having different airfoil sections, by David Biermann and Edwin P. Hartman [No. 650], p. 145 , The column strength of two extruded aluminum-alloy h-sections, by William R. Osgood and Marshall Holt [No. 656], p. 289 , The compressibility burble and the effect of compressibility on pressures and forces acting on an airfoil, by John Stack, W.F. Lindsey, and Robert E. Littell [No. 646], p. 73 , The effect of Nacelle-propeller diameter ratio on body interference and on propeller and cooling characteristics, by James G. McHugh and Eldridge H. Derring [No. 680], p. 727 , The effect of continuous weathering of light metal alloys used in aircraft, by Willard Mutchler [No. 663], p. 395 , The influence of directed air flow on combustion in a spark-ignition engine, by A.M. Rothrock and R.C. Spencer [No. 657], p. 313 , The knocking characteristics of fuels in relation to maximum permissible performance of aircraft engines, by A.M. Rothrock and Arnold E. Biermann [No. 655], p. 267 , Wind-tunnel investigation of N.A.C.A. 23012, 23021, 23030 airfoils with various sizes of split flap, by Carl J. Wenzinger and Thomas A. Harris [No. 668], p. 493 , Wind-tunnel investigation of an N.A.C.A. 23012 airfoil with a slotted flap and three types of auxiliary flap, by Carl J. Wenzinger and William E. Gauvain [No. 679], p. 699 , Wind-tunnel investigation of an N.A.C.A. 23021 airfoil with various arrangements of slotted flaps, by Carl J. Wenzinger and Thomas A. Harry [No. 677], p. 665 , Wind-tunnel investigation of an N.A.C.A. 23102 airfoil with various arrangements of slotted flaps, by Carl J. Wenzinger, and Thomas A. Harris [No. 664], p. 423 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (750 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. 10174

Note: A study of two-control operation of an airplane, by Robert T. Jones [No. 579], p. 73 , A theory of primary failure of straight centrally loaded columns, by Eugene E. Lundquist and Claude M. Fligg [No. 582], p. 141 , Air propellers in yaw, by E.P. Lesley, George F. Worley, and Stanley Moy [No. 597], p. 459 , Airfoil section characteristics as affected by variations of the Reynolds number, by Eastman N. Jacobs and Albert Sherman [No. 586], p. 227 , Alternating-current equipment for the measurement of fluctuations of air speed in turbulent flow, by W.C. Mock, Jr. [No. 598], p. 475 , An analysis of lateral stability in power-off flight with charts for use in design, by Charles H. Zimmerman [No. 589], p. 297 , An analysis of the factors that determine the periodic twist of an autogiro rotor blade, with a comparison of predicted and measured results, by John B. Wheatley [No. 600], p. 503 , An analytical and experimental study of the effect of periodic blade twist on the thrust torque, and flapping motion of an autogiro rotor, by John B. Wheatley [No. 591], p. 353 , Appendix, p. 159 , Blower cooling of finned cylinders, by Oscar W. Schey and Herman H. Ellerbrock, Jr. [No. 587], p. 269 , Characteristics of six propellers including the high-speed range, by Theodore Theodorsen, George W. Stickle, and M.J. Brevoort [No. 594], p. 401 , Cooling of airplane engine at low air speeds, by Theodore Theodorsen, M.J. Brevoort, and George W. Stickle [No. 593], p. 391 , Cooling test of a single-row radial engine with several N.A.C.A. cowlings, by M.J. Brevoort, George W. Stickle, and Herman H. Ellerbrock, Jr. [No. 596], p. 449 , Electrical thermometers for aircraft, by John B. Peterson and S.H.J. Womack [No. 606], p. 633 , Experimental investigation of wind-tunnel interference on the down wash behind an airfoil, by Abe Silverstein and S. Katzoff [No. 609], p. 689 , Flight measurements of the dynamic longitudinal stability of several airplanes and a correlation of the measurements with pilots' observations of handling characteristics, by Hartley A. Soule [No. 578], p. 69 , Flight tests of the drag and torque of the propeller in terminal-velocity dives, by Richard V. Rhode and Henry A. Pearson [No. 599], p. 493 , Fuel spray and flame formation in a compression-ignition engine employing airflow, by A.M. Rothrock and C.D. Waldron [No. 588], p. 281 , Full-scale tests of N.A.C.A. cowlings, by Theodore Theodorsen, M.J. Brevoort, and George W. Stickle [No. 592], p. 361 , Full-scale tests of a new type N.A.C.A. nose-slot cowling, by Theodore Theodorsen, M.J. Brevoort, George W. Stickle, and M.N. Gough [No. 595], p. 439 , Heat transfer to fuel sprays injected into heated gases, by Robert F. Selden and Robert C. Spencer [No. 580], p. 91 , Measurements of intensity and scale of wind-tunnel turbulence and their relation to the critical Reynolds number of spheres, by Hugh L. Dryden, G.B. Schubauer, W.C. Mock, Jr., and H.K. Skramstad [No. 581], p. 109 , Prechamber compression-ignition engine performance, by Charles S. Moore and John H. Collins, Jr. [No. 577], p. 49 , Pressure distribution measurements of an 0-2H airplane in flight, by H.A. Pearson [No. 590], p. 319 , Pressure-distribution measurements at large angles of pitch on fins of different span-chord ratio on a 1/40 scale model of the U.S. airship "Akron," by James G. McHugh [No. 604], p. 585 , Resume and analysis of N.A.C.A. lateral control research, by Fred E. Weick and Robert T. Jones [No. 605], p. 605 , Span load distribution for tapered wings with partial-span flaps, by H.A. Pearson [No. 585], p. 209 , Spinning characteristics of the XN2Y-1 airplane obtained from the spinning balance and compared with results from the spinning tunnel and from flight tests, by M.J. Bamber and R.O. House [No. 607], p. 649 , Strength of welded aircraft joints, by W.C. Brueggeman [No. 584], p. 177 , Stress analysis of beams with shear deformation of the flanges, by Paul Kuhn [No. 608], p. 669 , Table of contents, p. III , Tests of related forward-camber airfoils in the variable-density wind tunnel, by Eastman N. Jacobs, Robert M. Pinkerton, and Harry Greenberg [No. 610], p. 697 , The rolling friction of several airplane wheels and tires and the effect of rolling friction on take-off, by J.W. Wetmore [No. 583], p. 169 , Torsion tests of tubes, by Ambrose H. Stang, Walter Ramberg, and Goldie Back [No. 601], p. 515 , Wind-tunnel and flight tests of slot-lip ailerons, by Joseph A. Shortal [No. 563], p. 537 , Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps, by Carl J. Wenzinger [No. 611], p. 733 , Wind-tunnel investigation of wings with ordinary ailerons and full-span external airfoil flaps, by Robert C. Platt and Joseph A. Shortal [No. 603], p. 563 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (532 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. 10576

Note: A theoretical study of lateral stability with an automatic pilot, by Frederick H. Imlay, N.A.C.A. [No. 693], p. 273 , Aerodynamic characteristics of horizontal tail surfaces, by Abe Silverstein and S. Katzoff, N.A.C.A. [No. 688], p. 175 , Appendix, p. 80 , Correlation of cooling data from an air-cooled cylinder and several multicylinder engines, by Benjamin Pinkel and Herman H. Ellenbrock, Jr., N.A.C.A. [No. 683], p. 59 , Design charts relating to the stalling of tapered wings, by H.A. Soule and R.F. Anderson, N.A.C.A. [No. 703], p. 513 , Determination of ground effect from tests of a gilder in towed flight, by J.W. Wetmore and L.I. Turner, Jr., N.A.C.A. [No. 695], p. 295 , Effect of exit-slot position and opening on the available cooling pressure for N.A.C.A. nose-slot cowlings, by George W. Stickle, Irven Naiman, and John L. Crigler, N.A.C.A. [No. 687], p. 163 , Effect of fuel-air ratio, inlet temperature and exhaust pressure on detonation, by E.S. Taylor, W.A. Leary, and J.R. Diver, Massachusetts Institute of Technology [No. 699], p. 423 , Effective gust structure of low altitudes as determined from the reactions of an airplane, by Philip Donely, N.A.C.A. [No. 692], p. 263 , Flame speeds and energy considerations for explosions in a spherical bomb, by Ernest F. Fiock, Charles F. Marvin, Jr., Frank R. Caldwell, and Carl H. Roeder, N.A.C.A. [No. 682], p. 39 , Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. V. Effect of airplane relative density, by Oscar Seidman and A.I. Neihouse, N.A.C.A. [No. 691], p. 243 , Investigations on the incompletely developed plane diagonal-tension field, by Paul Kuhn, N.A.C.A. [No. 697], p. 387 , Longitudinal stability and control with special reference to slipstream effects, by S. Katzoff, N.A.C.A. [No. 690], p. 213 , Mechanical properties of flush-riveted joints, by W.C. Brueggeman and Frederick C. Roop, National Bureau of Standards [No. 701], p. 467 , Mechanism of flutter: A theoretical and experimental investigation of the flutter problem, by Theodore Theodorsen and I.E. Garrick, N.A.C.A. [No. 685], p. 101 , Piston temperatures in an air-cooled engine for various operating conditions, by Eugene J. Manganiello, N.A.C.A. [No. 698], p. 413 , Preliminary investigation of the flying qualities of airplanes, by H.A. Soule, N.A.C.A. [No. 700], p. 449 , Preliminary wind-tunnel investigation of an N.A.C.A. 23012 airfoil with various arrangements of Venetian-blind flaps, by Carl J. Wenzinger and Thomas A. Harris, N.A.C.A. [No. 689], p. 197 , Stability of castering wheels for aircraft landing gears, by Arthur Kantrowitz, N.A.C.A. [No. 686[, p. 147 , Static thrust and power characteristics of six full-scale propellers, by Edwin P. Hartman and David Biermann, N.A.C.A. [No. 684], p. 85 , Tensile elastic properties of typical stainless steels and nonferrous metals as affected by plastic deformation and by heat treatment, by D.J. McAdam, Jr., and R.W. Mebs, National Bureau of Standards [No. 696], p. 309 , The application of basic data on planing surfaces to the design of flying-boat hulls, by Walter S. Diehl, Bureau of Aeronautics, Navy Department [No. 694], p. 287 , The calculated effect of various hydrodynamic and aerodynamic factors on the take off of a large flying boat, by R.E. Olson and J.M. Allison, N.A.C.A. [No. 702], p. 497 , The unsteady lift of a wing of finite aspect ratio, by Robert T. Jones, N.AC.A. [No. 681), p. 31 , © 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)

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Format: Online-Ressource (987 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. 11554

Note: A radar method of calibrating airspeed installations on airplanes in maneuvers at high altitudes and at transonic and supersonic speeds, by John A. Zalcovcik [No. 985], p. 661 , An analysis of supersonic aerodynamic heating with continuous fluid injection, by E.B. Klunker and H. Reese Ivey [No. 990], p. 701 , An introduction to the physical aspects of helicopter stability, by Alfred Gessow and Kenneth B. Amer [No. 993], p. 739 , Analysis of spanwise temperature distribution in three types of air-cooled turbine blade, by John N.B. Livingood and W. Byron Brown [No. 994], p. 753 , Appendices, p. 100 , Application of radial-equilibrium condition to axial-flow compressor and turbine design, by Chung-Hua Wu and Lincoln Wolfenstein [No. 955], p. 165 , Attainable circulation about airfoils in cascade, by Arthur W. Goldstein and Artur Mager [No. 953], p. 117 , Blockage corrections for three-dimensional-flow closed-throat wind tunnels, with consideration of the effect of compressibility, by John G. Herriot [No. 995], p. 771 , Calculation of the aerodynamic loading of swept and unswept flexible wings of arbitrary stiffness, by Franklin W. Diederich [No. 1000], p. 909 , Comparative drag measurements at transonic speeds of rectangular and sweptback NACA 65-109 airfoils mounted on a freely falling body, by Charles W. Mathews and Jim Rogers Thompson [No. 988], p. 685 , Critical stress of ring-stiffened cylinders in torsion, by Manuel Stein, J. Lyell Sanders, Jr., and Harold Crate [No. 989], p. 693 , Determination of plate compressive strengths at elevated temperatures, by George J. Heimerl and William M. Roberts [No. 960], p. 251 , Direct method of design and stress analysis of rotating disks with temperature gradient, by S.S. Manson [No. 952], p. 103 , Elastic and plastic buckling of simply supported solid-core sandwich plates in compression, by Paul Seide and Elbridge Z. Stowell [No. 967], p. 357 , Equilibrium operating performance of axial-flow turbojet engines by means of idealized analysis, by John C. Sanders and Edward C. Chapin [No. 987], p. 673 , Flight investigation of the effect of various vertical-tail modifications on the directional stability and control characteristics of a propeller-driven fighter airplane, by Harold L. Johnson [No. 973], p. 453 , Flutter of a uniform wing with an arbitrarily placed mass according to a differential-equation analysis and a comparison with experiment, by Harry L. Runyan and Charles E. Watkins [No. 966], p. 339 , Free-space oscillating pressures near the tips of rotating propellers, by Harvey H. Hubbard and Arthur A. Regier [No. 996], p. 785 , Frequency response of linear systems from transient data, by Melvin E. Laverne and Aaron S. Boksenbom [No. 977], p. 547 , Fundamental effects of aging on creep properties of solution-treated low-carbon N-155 alloy, by D.N. Frey, J.W. Freeman, and A.E. White [No. 1001], p. 939 , Further experiments on the flow and heat transfer in a heated turbulent air jet, by Stanley Corrsin and Mahinder S. Uberoi [No. 998], p. 859 , General algebraic method applied to control analysis of complex engine types, by Aaron S. Boksenbom and Richard Hood [No. 980], p. 581 , Icing-protection requirements for reciprocating-engine induction systems, by Willard D. Coles, Vern G. Rollin, and Donald R. Mulholland [No. 982], p. 611 , Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings, by Alex Goodman and Lewis R. Fisher [No. 968], p. 367 , Investigation of the NACA 4-(3)(08)-03 and NACA 4-(3)(08)-045 two-blade propellers at forward mach numbers to 0.725 to determine the effects of compressibility and solidity on performance, by John B. Delano and Lewis Feldman [No. 999], p. 877 , Investigation with an interferometer of the turbulent mixing of a free supersonic jet, by Paul B. Gooderum, George P. Wood, and Maurice J. Brevoort [No. 963], p. 289 , Laminar mixing of a compressible fluid, by Dean R. Chapman [No. 958], p. 231 , Line-vortex theory for calculation of supersonic downwash, by Harold Mirels and Rudolph C. Haefeli [No. 983], p. 635 , Linear theory of boundary effects in open wind tunnels with finite jet lengths, by S. Katzoff, Clifford S. Gardner, Leo Diesendruck, and Bertram J. Eisenstadt [No. 976], p. 509 , Linearized compressible-flow theory for sonic flight speeds, by Max A. Heaslet, Harvard Lomax, and John R. Spreiter [No. 956], p. 195 , Method for determining the frequency-response characteristics of an element or system from the system transient output response to a known input function, by Howard J. Curfman, Jr. and Robert A. Gardiner [No. 984], p. 651 , Method of designing cascade blades with prescribed velocity distributions in compressible potential flows, by George R. Costello [No. 978], p. 559 , On stability of free laminar boundary layer between parallel streams, by Martin Lessen [No. 979], p. 571 , On the theory of oscillating airfoils of finite span in subsonic compressible flow, by Eric Reissner [No. 1002], p. 969 , One-dimensional flows of an imperfect diatomic gas, by A.J. Eggers [No. 959], p. 239 , Small bending and stretching of sandwich-type shells, by Eric Reissner [No. 975], p. 483 , Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip, by John D. Bird [No. 969], p. 379 , Summary of information relating to gust loads on airplanes, by Philip Donely [No. 997], p. 807 , Table of contents, p. II , The aerodynamic forces on slender plane and cruciform-wing and body combinations, by John R. Spreiter [No. 962], p. 271 , The application of Green's theorem to the solution of boundary-value problems in linearized supersonic wing theory, by Max A. Heaslet and Harvard Lomax [No. 961], p. 257 , The application of the statistical theory of extreme values to gust-load problems, by Harry Press [No. 991], p. 711 , The calculation of downwash behind supersonic wings with an application to triangular plan forms, by Harvard Lomax, Loma Sluder, and Max A. Heaslet [No. 957], p. 211 , The effect of torsional flexibility on the rolling characteristics at supersonic speeds of tapered unswept wings, by Warren A. Tucker and Robert L. Nelson [No. 972], p. 425 , The effects of variations in Reynolds Number between 3.0 X 10 [to the sixth power] and 2.5 X 10 [to the sixth power] upon the aerodynamic characteristics of a number of NACA 6-Series airfoil sections, by Laurence K. Loftin, Jr. and William J. Bursnall [No. 964], p. 307 , The longitudinal stability of elastic swept wings at supersonic speed, by C.W. Frick and R.S. Chubb [No. 965], p. 327 , The reversibility theorem for thin airfoils in subsonic and supersonic flow, by Clinton E. Brown [No. 986], p. 669 , The supersonic axial-flow compressor, by Arthur Kantrowitz [No. 974], p. 473 , Theoretical analysis of various thrust-augmentation cycles for turbojet engines, by Bruce T. Lundin [No. 981], p. 593 , Theoretical comparison of several methods of thrust augmentation for turbojet engines, by Eldon W. Hall and E. Clinton Wilcox [No. 992], p. 727 , Theoretical lift and damping in roll and supersonic speeds of thin sweptback tapered wings with streamwise tips, subsonic leading edges, and supersonic trailing edges, by Frank S. Malvestuto, Jr., Kenneth Margolis, and Herbert S. Ribner [No. 970], p. 395 , Theoretical stability derivatives of thin sweptback wings tapered to a point with sweptback or sweptforward trailing edges for a limited range of supersonic speeds, by Frank S. Malvestuto, Jr. and Kenneth Margolis [No. 971], p. 411 , Two-dimensional compressible flow in centrifugal compressors with straight blades, by John D. Stanitz and Gaylord O. Ellis [No. 954], p. 141 , Use of source distributions for evaluating theoretical aerodynamics of thin finite wings at supersonic speeds, by John C. Evvard [No. 951], p. 71 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: 1 online resource (18 pages, 6 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; no. 797

Note: "February 1941." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (18 pages, 6 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; no. 797

Note: "February 1941." , No Federal Depository Library Program (FDLP) item number.

Language: English