Kooperativer Bibliotheksverbund

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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)

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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 (799 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. 9348

Note: A method of calculating the ultimate strength of continuous beams, by J.A. Newlin and George W. Trayer [No. 347], p. 291 , A proof of the theorem regarding the distribution of lift over the span for minimum induced drag, by W.F. Durand [No. 349], p. 361 , Aircraft accidents: Method of analysis, by Committee on Aircraft Accidents of the National Advisory Committee for Aeronautics [No. 357], p. 539 , Aircraft woods: Their properties, selection, and characteristics, by L.J. Markwardt [No. 354], p. 467 , Airfoil pressure distribution investigation in the variable density wind tunnel, by Eastman N. Jacobs, John Stack, and Robert M. Pinkerton [No. 353], p. 451 , An extended theory of thin airfoils and its application to the biplane problem, by Clark B. Millikan [No. 362], p. 635 , An investigation of the effectiveness of ignition sparks, by Melville F. Peters, Wayne L. Summerville, and Merlin Davis [No. 359], p. 573 , Comparative flight performance with an N.A.C.A. roots supercharger and a turbocentrifugal supercharger, by Oscar W. Schey and Alfred W. Young [No. 355], p. 501 , Effect of turbulence in wind tunnel measurements, by H.L. Dryden and A.M. Kuethe [No. 342], p. 145 , Effect of variation of chord and span of ailerons on rolling and yawing moments at several angles of pitch, by R.H. Heald, D.H. Strother, and B.H. Monish [No. 343], p. 171 , Experimental determination of jet boundary corrections for airfoil tests in four open wind tunnel jets of different shapes, by Montgomery Knight and Thomas A. Harris [No. 361], p. 607 , Full scale wind tunnel tests of a propeller with the diameter changed by cutting off the blade tips, by Donald H. Wood [No. 351], p. 393 , Full scale wind tunnel tests on several metal propellers having different blade forms, by Fred E. Weick [No. 340], p. 121 , Full scale wind tunnel tests with a series of propellers of different diameters on a single fuselage, by Fred E. Weick [No. 339], p. 105 , Large scale aerodynamic characteristics of airfoils as tested in the variable density wind tunnel, by Eastman N. Jacobs and Raymond F. Anderson [No. 352], p. 419 , List of technical reports, p. VII , Pressure distribution over a symmetrical airfoil section with trailing edge flap, by Eastman N. Jacobs and Robert M. Pinkerton [No. 360], p. 587 , Pressure fluctuations in a common-rail fuel injection system, by A.M. Rothrock [No. 363], p. 669 , Strength of rectangular flat plates under edge compression, by Louis Schuman and Goldie Black [No. 356], p. 515 , Strength of welded joints in tubular members for aircraft, by H.L. Whittemore and W.C. Brueggeman [No. 348], p. 319 , Table of contents, p. VI , Temperature coefficient of the modulus of rigidity of aircraft instrument diaphragm and spring materials, by W.G. Brombacher and E.R. Melton [No. 358], p. 557 , The design and development of an automatic injection valve with an annular orifice of varying area, by William F. Joachim, Chester W. Hicks, and Hampton H. Foster [No. 341], p. 135 , The design of airplane wing ribs, by J.A. Newlin and George W. Trayer [No. 345], p. 219 , The design of plywood webs for airplane wing beams, by George W. Trayer [No. 344], p. 201 , The effect of reduction gearing on propeller-body interference as shown by full scale wind tunnel tests, by Fred E. Weick [No. 338], p. 83 , The gaseous explosive reaction at constant pressure -- the reaction order and reaction rate, by F.W. Stevens [No. 337], p. 67 , The pressure distribution over the wings and tail surfaces of a PW-9 pursuit airplane in flight, by Richard V. Rhode [No. 364], p. 685 , Water pressure distribution on a flying boat hull, by F.L. Thompson [No. 346], p. 273 , Working charts for the selection of aluminum alloy propellers of a standard form to operate with various aircraft engines and bodies, by Fred E. Weick [No. 350], p. 377 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)