Kooperativer Bibliotheksverbund

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Format: Online-Ressource (657 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. 9911

Note: A description and test results of a spark-ignition and a compression-ignition 2-stroke cycle engine, by J.A. Spanogle and E.G. Whitney [No. 495], p. 395 , A flight investigation of the effect of mass distribution and control setting on the spinning of the XN2Y-1 airplane, by N.F. Scudder [No. 484], p. 185 , A flight investigation of the lateral control characteristics of short wide ailerons and various spoilers with different amounts of wing dihedral, by Fred E. Weick, Hartley A. Soule, and Melvin N. Gough [No. 494], p. 381 , Air conditions close to the ground and the effect on airplane landings, by F.L. Thompson, W.C. Peck, and A.P. Beard [No. 489], p. 271 , An aerodynamic analysis of the autogiro rotor with a comparison between calculated and experimental results, by John B. Wheatley [No. 487], p. 235 , Computation of the two-dimensional flow in a laminar boundary layer, by Hugh L. Dryden [No. 497], p. 435 , Effect of moderate air flow on the distribution of fuel sprays after injection cut-off, by A.M. Rothrock and R.C. Spencer [No. 483], p. 163 , Effect of viscosity on fuel leakage between lapped plungers and sleeves and on the discharge from a pump-injection system, by A.M. Rothrock and E.T. Marsh [No. 477], p. 63 , Experimental verification of the theory of wind-tunnel boundary interference, by Theodore Theodorsen and Abe Silverstein [No. 478], p. 79 , General theory of aerodynamic instability and the mechanism of flutter, by Theodore Theodorsen [No. 496], p. 413 , Heat transfer from finned metal cylinders in an air stream, by Arnold E. Biermann and Benjamin Pinkel [No. 488], p. 251 , Improved airplane windshields to provide vision in stormy weather, by William C. Clay [No. 498], p. 445 , Infrared radiation from explosions in a spark-ignition engine, by Charles F. Marvin, Jr., Frank R. Caldwell, and Sydney Steele [No. 486], p. 223 , List of technical reports, p. VII , On the theory of laminar boundary layers involving separation, by Th. von Karman and C.B. Milliken [No. 504], p. 541 , Relation of hydrogen and methane to carbon monoxide in exhaust gases from internal combustion engines, by Harold C. Gerrish and Arthur M. Tessmann [No. 476], p. 53 , Relative loading on biplane wings of unequal chords, by Walter S. Diehl [No. 501], p. 503 , Scale effect on Clark V airfoil characteristics from N.A.C.A. full-scale wind-tunnel tests, by Abe Silverstein [No. 502], p. 509 , Stability of thin-walled tubes under torsion, by L.H. Donnell [No. 479], p. 95 , Tests of nacelle-propeller combinations in various positions in reference to wings. IV. -- Thick wing -- various radial engine cowlings -- tandem propellers, by James G. McHugh [No. 505], p. 561 , Tests of 16 related airfoils at high speeds, by John Stack and Albert B. von Doenhoff [No. 492], p. 339 , Tests of nacelle-propeller combinations in various positions in reference to wings. V. -- Clark Y biplane cellule -- N.A.C.A. cowled nacelle -- tractor propeller, by E. Floyd Valentine [No. 506], p. 603 , Tests of nacelle-propeller combinations in various positions with reference to wings. VI. -- Wings and nacelles with pusher propeller, by Donald H. Wood and Carlton Bioletti [No. 507], p. 619 , The aerodynamic effects of wing cut-outs, by Albert Sherman [No. 480], p. 117 , The drag of airplane wheels, wheel fairings, and landing gears-I, by William H. Herrnstein, Jr. and David Biermann [No. 485], p. 193 , The effect of spray strips on the take-off performance of a model of a flying boat hull, by Starr Truscott [No. 503], p. 523 , The influence of tip shape on the wing-load distribution as determined by flight tests, by Richard V. Rhode [No. 500], p. 479 , The physical effects of detonation in a closed cylindrical chamber, by C.S. Draper [No. 493], p. 361 , The weathering of aluminum alloy sheet materials used in aircraft, by Willard Mutchler [No. 490], p. 285 , Vibration response of airplane structures, by T. Theodorsen and A.G. Gelalles [No. 491], p. 319 , Wind tunnel research comparing lateral control devices, particularly at high angles of attack. XII. -- Upper surface ailerons on wings with split flaps, by Fred E. Weick and Carl J. Wenzinger [No. 499], p. 463 , Wing pressure distribution and rotor-blade motion of an autogiro as determined in flight, by John B. Wheatley [No. 475], p. 43 , Wing-fuselage interference, tail buffeting, and air flow about the tail of a low-wing monoplane, by James A. White and Manley J. Hood [No. 482], p. 143 , Working charts for the determination of propeller thrust at various air speeds, by Edwin P. Hartman [No. 481], p. 123 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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

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

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

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

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (756 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. 9667

Note: A method for computing leading-edge loads, by Richard V. Rhode and Henry A. Pearson [No. 413], p. 249 , Aircraft speed instruments, by K. Hilding Beij [No. 420], p. 381 , Appendix, p. 237 , Application of practical hydrodynamics to airship design, by Ralph H. Upson and W.A. Klikoff [No. 405], p. 123 , Characteristics of Clark Y airfoils of small aspect ratios, by C.H. Zimmerman [No. 431], p. 581 , Combustion in a high-speed compression-ignited engine, by A.M. Rothrock [No. 401], p. 63 , Drop and flight tests on NY-2 landing gears including measurements of vertical velocities at landing, by W.C. Peck and A.P. Beard [No. 406], p. 141 , Effect of orifice length-diameter ratio on fuel sprays for compression-ignition engines, by A.G. Gelalles [No. 402], p. 79 , Experiments on the distribution of fuel in fuel sprays, by Dana W. Lee [No. 438], p. 703 , Force measurements on a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 432], p. 591 , Fuel vaporization and its effect on combustion in a high-speed compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 435], p. 629 , General formulas and charts for the calculation of airplane performance, by W. Bailey Oswald [No. 408], p. 163 , Ice prevention on aircraft by means of engine exhaust heat and a technical study of heat transmission from a Clark Y airfoil, by Theodore Theodorsen and William C. Clay [No. 403], p. 91 , Lift and drag characteristics and gliding performance of an autogiro as determined in flight, by John B. Wheatley [No. 434], p. 621 , Measurement of the differential and total thrust and torque of six full-scale adjustable-pitch propellers, by George W. Stickle [No. 421], p. 437 , Measurements of flow in the boundary layer of a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 430], p. 567 , Preliminary investigation of modifications to conventional airplanes to give nonstalling and short-landing characteristics, by Fred E. Weick [No. 418], p. 343 , Pressure distribution tests on a series of Clark Y biplane cellules with special reference to stability, by Richard W. Noyes [No. 417], p. 315 , Rates of fuel discharge as affected by the design of fuel-injection systems for internal-combustion engines, by A.G. Gelalles and E.T. Marsh [No. 433], p. 607 , Table of contents, p. VII , Tests of nacelle-propeller combinations in various positions with reference to wings. Part I. Thick wing -- N.A.C.A. cowled nacelle-tractor propeller, by Donald H. Wood [No. 415], p. 277 , Tests on nacelle-propeller combinations in various positions with reference to wings. II. -- Thick wing -- various radial-engine cowlings -- tractor propeller, by Donald H. Wood [No. 436], p. 653 , The 7 by 10 foot wind tunnel of the National Advisory Committee for Aeronautics, by Thomas A. Harris [No. 412], p. 241 , The N.A.C.A. apparatus for studying the formation and combustion of fuel sprays and the results from preliminary tests, by A.M. Rothrock [No. 429], p. 549 , The N.A.C.A. variable-density wind tunnel, by Eastman N. Jacobs and Ira H. Abbott [No. 416], p. 305 , The characteristics of a Clark Y wing model equipped with several forms of low-drag fixed slots, by Fred E. Weick and Carl J. Wenzinger [No. 407], p. 155 , The effect of area and aspect ratio on the yawing moments of rudders at large angles of pitch on three fuselages, by Hugh L. Dryden and B.H. Monish [No. 437], p. 693 , The effect of humidity on engine power at altitude, by D.B. Brooks and E.Z. Garlock [No. 426], p. 523 , The effect of increased carburetor pressure on engine performance at several compression ratios, by Oscar W. Schey and Vern G. Rollin [No. 404], p. 113 , The effect of multiple fixed slots and a trailing-edge flap on the lift and drag of a Clark Y airfoil, by Fred E. Weick and Joseph A. Shortal [No. 427], p. 531 , The effect of nozzle design and operating conditions on the atomization and distribution of fuel sprays, by Dana W. Lee [No. 425], p. 505 , The effect on airplane performance of the factors that must be considered in applying low-drag cowling to radial engines, by William H. McAvoy, Oscar W. Schey, and Alfred W. Young [No. 414], p. 259 , The elimination of fire hazard due to back fires, by Theodore Theodorsen and Ira M. Freeman [No. 409], p. 211 , The mechanism of atomization accompanying solid injection, by R.A. Castleman, Jr. [No. 440], p. 735 , The theory of wind-tunnel wall interference, by Theodore Theodorsen [No. 410], p. 219 , Theory of wing sections of arbitrary shape, by Theodore Theodorsen [No. 411], p. 229 , Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. I. -- Ordinary ailerons on rectangular wings, by Fred E. Weick and Carl J. Wenzinger [No. 419], p. 357 , Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. II. -- Slotted ailerons and Frise ailerons, by Fred E. Weick and Richard W. Noyes [No. 422], p. 457 , Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. III. -- Ordinary ailerons rigged up 10 [degrees] when neutral, by Fred E. Weick and Carl J. Wenzinger [No. 423], p. 471 , Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. IV. -- Floating tip ailerons on rectangular wings, by Fred E. Weick and Thomas A. Harris [No. 424], p. 481 , Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. V. -- Spoilers and ailerons on rectangular wings, Fred E. Weick and Joseph A. Shortal [No. 439], p. 719 , Wind-tunnel tests of a Clark Y wing with a narrow auxiliary airfoil in different positions, by Fred E. Weick and Millard J. Bamber [No. 428], p. 537 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: 1 online resource (7 pages, 8 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 394

Note: "October, 1931. , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (7 pages, 8 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 394

Note: "October, 1931. , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (21 pages, 12 unnumbered pages) : , illustrations.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 339

Note: "May, 1930." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (15 pages, 19 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 604

Note: "July 1937." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (15 pages, 19 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 604

Note: "July 1937." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (21 pages, 12 unnumbered pages) : , illustrations.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 339

Note: "May, 1930." , No Federal Depository Library Program (FDLP) item number.

Language: English