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Synonyms were used for: Theorie
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    Method of designing airfoils with prescribed velocity distributions in compressible potential flows

    Costello, George R | NTRS | 1949
    Keywords: THEORIES - AIRFOILS , THEORIES - AIRFOILS CASCADES

    Method for Caluculating Lift Distributions for Unswept Wings with Flaps or Ailerons by use of Nonlinear Section Lift Data

    Sivells, James C / Westrick, Gertrude C | NTRS | 1951
    Keywords: WINGS, COMPLETE - THEORY

    Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls

    Dannenberg, Robert E | NTRS | 1950
    Keywords: THEORIES - WINGS

    LUNAR LANDING AND LONG-RANGE EARTH REENTRY GUIDANCE BY APPLICATION OF PERTURBATION THEORY

    Coate, R. E. / Lessing, H. C. / Tunnell, P. J. | NTRS | 1963
    Keywords: PERTURBATION THEORY

    Load distributions due to steady roll and pitch for thin wings at supersonic speeds

    Moeckel, W E / Evvard, J C | NTRS | 1948
    Keywords: THEORIES - FLOW SUPERSONIC , THEORIES - WINGS

    Linearized lifting-surface theory for swept-back wings with slender plan forms

    Lomax, Harvard / Heaslet, Max A | NTRS | 1949
    Keywords: THEORIES - WINGS , THEORIES - FLOW - LINEAR , THEORIES - AIRFOILS - LIFTING-SURFACE

    Limitations of lifting-line theory for estimation of aileron hinge-moment characteristics

    Gillis, Clarence L | NTRS | 1943
    Keywords: THEORIES-AIRFOILS LIFTING-LINE

    Landing and Braking of Airplanes

    Breguet, Louis | NTRS | 1929
    Keywords: AIRPLANES - DESIGN & THEORY

    Jet-boundary-induced-upwash velocities for swept reflection-plane models mounted vertically in 7- by 10-foot, closed, rectangular wind tunnels

    Polhamus, Edward C | NTRS | 1948
    Keywords: THEORIES - VORTEX WINGS

    Jet-boundary corrections for reflection-plane models in rectangular wind tunnels

    Toll, Thomas A | NTRS | 1943
    Keywords: THEORIES - AIRFOILS - LIFTING-LINE

    Investigation of Wing Characteristics at a Mach Number of 1.53 II : Swept Wings of Taper Ratio 0.5

    Vincenti, Walter G / Van Dyke, Milton D / Matteson, Frederick H | NTRS | 1948
    Keywords: WINGS, COMPLETE - THEORY

    Information requirements for guidance and control systems

    Dawson, C. H. / Foy, W. H., Jr. / Larson, R. E. et al. | NTRS | 1966
    Keywords: INFORMATION THEORY

    Influence of leading-edge suction on lift-drag ratios of wings at supersonic speeds

    Cohen, Clarence B | NTRS | 1948
    Keywords: THEORIES - FLOW LINEAR

    Influence of fuselage on propeller design

    Troller, Theodor | NTRS | 1928
    Keywords: PROPELLERS - DESIGN & THEORY

    Improvements on the analysis of shells of revolution by the matrix displacement method.

    Navaratna, D. R. / Pian, T. H. H. / Stricklin, J. A. | NTRS | 1966
    Keywords: SHELL THEORY

    Impact theory for seaplane landings

    Benscoter, S U | NTRS | 1947
    Keywords: THEORIES - IMPACT

    Heat transfer to bodies traveling at high speed in the upper atmosphere

    Stalder, Jackson, R / Jukoff, David | NTRS | 1948
    Keywords: THEORIES - GASES

    Heat-transfer processes in liquid-cooled engine cylinders I : correlation of single-cylinder engine temperatures under forced-convection cooling conditions

    Bernardo, Everett | NTRS | 1946
    Keywords: THEORIES-HEAT TRANSMISSION

    Geodetic information and implications

    Okeefe, J. | NTRS | 1964
    Keywords: GRAVITATION THEORY

    GENERAL THEORY OF PERSONNEL DECISION

    Brady, J. S. | NTRS | 1963
    Keywords: PROBABILITY THEORY

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