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    Zur Frage der selbsterregten Fuegelschwingungen

    von Schlippe, B. | Engineering Index Backfile | 1936
    Publisher: National Advisory Committee for Aeronautics

    Zur entstehung des luftschraubengeraeusches

    Ernsthausen, W. | Engineering Index Backfile | 1937
    Publisher: National Advisory Committee for Aeronautics

    Zunkunftsfragen des Segelfluges

    Georgii, W. | Engineering Index Backfile | 1933
    Zeit fuer Flugtechnik und Motorluftschiffahrt v 24 n 5 Mar 14 1933 p 125-35 (discussion) p 135-6) ...
    Publisher: National Advisory Committee for Aeronautics

    Zero-lift wave drag of particular family of unswept, tapered wings with linearly varying thickness ratio

    Henderson, Jr., A. / Goodwin, J.M. | Engineering Index Backfile | 1955
    Publisher: National Advisory Committee for Aeronautics

    Zero-lift drag of slender body of revolution (NACA RM-10 Research Model) as determined from tests in several wind tunnels and in flight at supersonic speeds

    Evans, A.J. | Engineering Index Backfile | 1954
    Publisher: National Advisory Committee for Aeronautics

    Zero-lift Drag of 60° Delta-wing -- Body combination (AGARD Model 2) obtained from free-flight tests between mach numbers of 0.8 and 1.7

    Piland, R.O. | Engineering Index Backfile | 1954
    Publisher: National Advisory Committee for Aeronautics

    X-57 Maxwell Airworthiness Validation Plan

    Herbert W Schlickenmaier / Mark Anderson / Evan Harrison et al. | NTRS | 2023
    methods of compliance from appropriate Federal Aviation Administration (FAA) Advisory Circulars and other sources to use for the X-57 Mod IV ...
    Publisher: NASA National Aeronautics and Space Administration

    Workshop notes on the building of metal hulls

    Langley, M. | TIBKAT | 1928
    Publisher: National Advisory Committee for Aeronautics , Washington, DC

    Working charts for the selection of aluminum alloy propellers of a standard form to operate with various aircraft engines and bodies

    Weick, F.E. | Engineering Index Backfile | 1931
    Charts prepared from full-scale test data obtained in 20-ft. propeller research tunnel; example for use is also given. ...
    Publisher: National Advisory Committee for Aeronautics

    Working charts for determination of propeller thrust at various air speeds

    Hartman, E.P. | Engineering Index Backfile | 1934
    Publisher: National Advisory Committee for Aeronautics

    Working charts for determination of lift distribution between biplane wings

    Kuhn, P. | Engineering Index Backfile | 1932
    dihedral in upper and lower wings may be properly provided for by utilizing concepts of average stagger and average gap/chord ratio. ...
    Publisher: National Advisory Committee for Aeronautics

    With a View to Their Practical Solution: Sixty Years with Naca and NASA, 1915 - 1976

    E. M. Emme | NTIS | 1976
    The history of the National Advisory Committee for Aeronautics and the National Aeronautics and Space Administration is examined. ...
    Publisher: National Aeronautics and Space Administration, Washington, DC

    With a view to their practical solution: Sixty years with NACA and NASA, 1915 - 1976

    Emme, E. M. | NTRS | 1976
    The history of the National Advisory Committee for Aeronautics and the National Aeronautics and Space Administration is examined. ...
    Publisher: NASA National Aeronautics and Space Administration

    Wings with nozzle-shaped slots

    Katzmayr, R. | Engineering Index Backfile | 1929
    employed in ordinary flight; drag values only little greater than for wings of simpler construction; number and location of slots in wing profile ...
    Publisher: National Advisory Committee for Aeronautics

    Wing spread as the basic factor in design

    Lachmann, G. | Engineering Index Backfile | 1928
    Effect of span on climbing ability of biplanes; study of maneuverability of airplane of great importance for judging combat, sport, and ...

    Wing pressure-distribution measurements up to 0,866 Mach number in flight on jet-propelled airplane

    Brown, H.H. / Clousing, L.A. | Engineering Index Backfile | 1947
    ; for lift coefficients ranging from 0 to 0.60, no appreciable compressibility effects on spanwise wing loading were noted below 0.75 Mach ...
    Publisher: National Advisory Committee for Aeronautics

    Wing pressure distribution and rotor-blade motion of autogiro as determined in flight

    Wheatley, J.B. | Engineering Index Backfile | 1933
    Publisher: National Advisory Committee for Aeronautics