Synonyms were used for: aircraft conference design lift
Search without synonyms: title: Vertical lift aircraft design conference

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    Compilation of papers presented by NACA staff members

    Engineering Index Backfile | 1946
    Research Investigations of Interest in Personal Aircraft Design, H. C. CHANDLER, Jr. ...

    Review of the Xb-70 Flight Program

    Thomas R. Sisk / Kirk S. Irwin / James M. McKay | NTRS | 1965
    generally substantiated predictions and indicate no unforeseen problems for this class of vehicle. Vertical velocities at impact are of the same ...
    Keywords: Aircraft Design, Testing And Performance

    Supplement to Conference Proceedings No. 22 Pre-Print

    NTIS | 1967
    Keywords: Vertical takeoff aircraft , Aircraft noise , Helicopter design , Lift drag ratio

    V/STOL Conference, Palo Alto, Calif., June 6-8, 1977, Technical Papers

    NTRS | 1977
    -lift STOL ground effects, conceptual design studies of Navy Type A V/STOL aircraft, and a V/STOL shaft propulsion system analytical performance ...
    Keywords: Aircraft Design, Testing And Performance

    Large lighter-than-air vehicles

    Mayer, N. J. | NTRS | 1979
    . These are in heavy vertical lift and in long endurance patrol. The most promising concepts for these missions include hybrid combinations of ...
    Keywords: Aircraft Design, Testing And Performance

    Type 'A' V/STOL - One aircraft for all support missions

    Adelt, W. H. | NTRS | 1981
    attack, and aspects of combat, search, and rescue. With the aid of a sample design for a V/STOL aircraft with a medium disc loading lift system ...
    Keywords: Aircraft Design, Testing And Performance

    Concept definition and aerodynamic technology studies for single-engine V/STOL fighter/attack aircraft

    Nelms, W. P. / Durston, D. A. | NTRS | 1981
    contractors have identified promising concepts featuring a variety of approaches for providing propulsive lift. Vertical takeoff gross weights range ...
    Keywords: Aircraft Design, Testing And Performance

    Analysis of selected VTOL concepts for a civil transportation mission

    Wilson, S. B., III / Bowles, J. V. / Foster, J. D. | NTRS | 1981
    study are the tilt jet concept utilizing rotating turbofan engines for both vertical lift and cruise thrust, and the tilt rotor concept using ...
    Keywords: Aircraft Design, Testing And Performance

    A Parametric Evaluation of Supersonic STOVL

    Rapp, David C. / Kidwell, George H. | SAE Technical Papers | 1985
    /attack aircraft design. The variables considered involved thrust vectoring, thrust degradation, maximum lift, and other changes to determine the ...
    Keywords: Aircraft

    X-Wing: A Low Disc-Loading V/STOL for the Navy

    Linden, Arthur W. / Biggers, James C. | SAE Technical Papers | 1985
    to design, fabricate, and flight test a full-scale X-Wing rotor/wing on the NASA/Army Rotor Systems Research Aircraft (RSRA). To date, detail ...
    Keywords: Vertical take-off and landing (VTOL) , Aircraft

    Takeoff Predictions for Powered-Lift Aircraft

    Hahn, Andrew S. / Sandlin, Doral R. / Wardwell, Douglas A. | SAE Technical Papers | 1986
    Takeoff predictions for powered lift short takeoff (STO) aircraft have been added to NASA AMES Research Center's aircraft synthesis (ACSYNT ...
    Keywords: Aircraft

    Lift Engines — Applied History

    Harvey, H. M. | SAE Technical Papers | 1987
    partly provided by lift engines designed for the purpose. A number of sophisticated experimental aircraft of this type were built and flown in ...
    Keywords: Vertical take-off and landing (VTOL) , Fixed-wing aircraft , Aircraft

    Integrated Control and Display Research for Transition and Vertical Flight on the NASA V/STOL Research Aircraft (VSRA)

    Moralez, Ernesto / Franklin, James A. / Schroeder, Jeffrey A. et al. | SAE Technical Papers | 1987
    flight to establish their value for advanced short takeoff vertical landing (STOVL) aircraft designs. This paper summarizes analytical studies ...
    Keywords: Aircraft

    STOVL RCS Effects on Propulsion System Design

    Coons, Lee | SAE Technical Papers | 1987
    Vertical landing/takeoff candidate aircraft will require some type of Reaction Control System (RCS) for aircraft balance, control, and ...
    Keywords: Aircraft

    Model 276 = STOVL Aircraft for Sea-Based Multimission Tactical-Sypport Roles - An Alternative

    Doerr, F. J. | SAE Technical Papers | 1987
    operational deployment freedom and basing flexibility could be achieved with a Short Takeoff and Vertical Landing (STOVL) aircraft under preliminary ...
    Keywords: Aircraft

    Overview of the US/UK ASTOVL Program

    Armstrong, Frank W. / Levine, Jack | SAE Technical Papers | 1987
    advantages of short take-off and vertical landing combined with supersonic performance and high agility in a future combat aircraft are very ...
    Keywords: Aircraft

    Configuration E-7 Supersonic STOVL Fighter/Attack Technology Program

    Sheridan, Arthur E. / Jenista, John E. | SAE Technical Papers | 1987
    described. This aircraft uses the ejector principle to augment engine fan air for vertical lift. The initial design objectives selected in 1980 are ...
    Keywords: Aircraft

    Integrated control and display research for transition and vertical flight on the NASA V/STOL Research Aircraft (VSRA)

    Foster, John D. / Moralez, Ernesto, III / Franklin, James A. et al. | NTRS | 1988
    flight to establish their value for advanced short takeoff vertical landing (STOVL) aircraft designs. This paper summarizes analytical studies ...
    Keywords: Aircraft Stability And Control

    Flight testing a V/STOL aircraft to identify a full-envelope aerodynamic model

    Mcnally, B. David / Bach, Ralph E., Jr. | NTRS | 1988
    aircraft, the YAV-8B Harrier. The flight envelope to be modeled includes hover, transition to conventionally flight and back to hover, STOL ...
    Keywords: Aircraft Design, Testing And Performance

    Proceedings - Vertical Lift Aircraft Design Conference, Sheraton Hotel at Fisherman's Wharf, San Francisco, California, January 17 - 19, 1990

    Vertical Lift Aircraft Design Conference / American Helicopter Society / Ames Research Center | TIBKAT | 1990