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  • 1
    UID:
    b3kat_BV024266918
    Language: Undetermined
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  • 2
    UID:
    gbv_440160553
    Format: XII, 434 S. : 1 Portr., graph. Darst.
    Uniform Title: Festschrift
    Note: Literaturangaben
    Language: Undetermined
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  • 3
    UID:
    gbv_754136612
    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)
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  • 4
    UID:
    gbv_754162117
    Format: Online-Ressource (583 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. 10106
    Note: A simplified application of the method of operators to the calculation of disturbed motions of an airplane, by Robert T. Jones [No. 560], p. 313 , Aerodynamic characteristics of N.A.C.A. 23012 and 23021 airfoils with 20-percent-chord external-airfoil flaps of N.A.C.A. 23012 section, by Robert C. Platt and Ira H. Abbott [No. 573], p. 523 , Air flow around finned cylinders, by M.J. Brevoort and Vern G. Rollin [No. 555], p. 237 , Air flow in the boundary layer near a plate, by Hugh L. Dryden [No. 562], p. 339 , Aircraft accidents method of analysis, report prepared by committee on aircraft accidents [No. 576], p. 564 , Aircraft compass characteristics, by John B. Peterson and Clyde W. Smith [No. 551], p. 187 , Calculated and measured pressure distributions over the midspan section of the N.A.C.A. 4412 airfoil, by Robert M. Pinkerton [No. 563], p. 365 , Combustion in a bomb with a fuel-injection system, by Mildred Cohn and Robert C. Spencer [No. 544], p. 107 , Cooling characteristics of a 2-row radial engine, by Oscar W. Schey and Vern G. Rollin [No. 550], p. 177 , Determination of the characteristics of tapered wings, by Raymond F. Anderson [No. 572], p. 503 , Effect of nozzle design on fuel spray and flame formation in a high-speed compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 561], p. 327 , Effect of tip shape and dihedral on lateral-stability characteristics, by Joseph A. Shortal [No. 548], p. 149 , Effects of air-fuel ratio on fuel spray and flame formation in a compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 545], p. 119 , Further studies of flame movement and pressure development in an engine cylinder, by Charles F. Marvin, Jr., Armistead Wharton, and Carl H. Roeder [No. 556], p. 251 , Ground-handling forces on a 1/40-scale model of the U.S. airship "Akron," by Abe Silverstein and B.G. Gulick [No. 566], p. 405 , Interference of wing and fuselage from tests of 28 combinations in the N.A.C.A. variable-density tunnel, by Albert Sherman [No. 575], p. 555 , List of technical reports, p. III , Measurements of fuel distribution within sprays for fuel-injection engines, by Dana W. Lee [No. 565], p. 389 , Potential flow about arbitrary biplane wing sections, by I.E. Garrick [No. 542], p. 47 , Preliminary tests in the N.A.C.A. free-spinning wind tunnel, by C.H. Zimmerman [No. 557], p. 265 , Pressure distribution over a rectangular airfoil with a partial-span split flap, by Carl J. Wenzinger and Thomas A. Harris [No. 571], p. 491 , Pressure distribution over an airfoil section with a flap and tab, by Carl J. Wenzinger [No. 574], p. 543 , Propulsion of a flapping and oscillating airfoil, by I.E. Garrick [No. 567], p. 419 , Some effects of argon and helium upon explosions of carbon monoxide and oxygen, by Ernest F. Fiock and Carl H. Roeder [No. 553], p. 213 , Tank tests of N.A.C.A. model 40 series of hulls for small flying boats and amphibians, by John B. Parkinson and John R. Dawson [No. 543], p. 77 , Tests of a wing-nacelle-propeller combination at several pitch settings up to 42℗ʻ, by Ray Windler [No. 564], p. 381 , The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data, by Fred E. Weick and Robert T. Jones [No. 570], p. 465 , The effect of turbulence on the drag of flat plates, by G.B. Schubauer and H.L. Dryden [No. 546], p. 129 , The forces and moments acting on parts of the XN2Y-1 airplane during spins, by N.F. Scudder [No. 559], p. 305 , The quiescent-chamber type compression-ignition engine, by H.H. Foster [No. 568], p. 429 , Turbulence factors of N.A.C.A. wind tunnels as determined by sphere tests, by Robert C. Platt [No. 558], p. 283 , Wind-tunnel interference with particular reference to off-center positions of the wing and to the downwash at the tail, by Abe Silverstein and James A. White [No. 547], p. 135 , Wind-tunnel investigation of ordinary and split flaps on airfoils of different profile, by Carl J. Wenzinger [No. 554], p. 223 , Wind-tunnel investigation of the aerodynamic balancing of upper-surface ailerons and split flaps, by Carl J. Wenzinger [No. 549], p. 159 , Wind-tunnel tests of 10-foot-diameter auto-giro rotors, by John B. Wheatley and Carlton Bioletti [No. 552], p. 199 , Wing-nacelle-propeller interference for wings of various spans force and pressure-distribution tests, by Russel G. Robinson and William H. Herrnstein, Jr. [No. 569], p. 449 , © 2008 by NewsBank, Inc. All rights reserved
    Language: English
    URL: Volltext  (Deutschlandweit zugänglich)
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