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

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    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

    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

    Volantor* - A Powered Lift Aircraft for Personal Use

    Moller, Paul S. | SAE Technical Papers | 2005
    This paper describes a class of “powered liftaircraft called volantors that utilize multiple ducted fans for generating thrust. Thrust is ...
    Keywords: Aircraft

    Vertical Lift - Not Just For Terrestrial Flight

    Young, Larry A | NTRS | 2000
    Autonomous vertical lift vehicles hold considerable potential for supporting planetary science and exploration missions. This paper ...
    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

    Trust Control of VTOL Aircraft Part Deux

    Dugan, Daniel C. | NTRS | 2014
    Thrust control of Vertical Takeoff and Landing (VTOL) aircraft has always been a debatable issue. In most cases, it comes down to the ...
    Keywords: Aircraft Design, Testing And Performance , Aircraft controls , VTOL Aircraft

    Trajectory computation Infrastructure based on BADA Aircraft Performance Model

    Gallo, Eduardo / Lopez-Leones, Javier / Vilaplana, Miguel A. et al. | IEEE | 2007
    the “aircraft intent” (AI). Three of them set the position of the landing gear, high lift devices, and speed brakes, while the ...

    The selection of convertible engines with current gas generator technology for high speed rotorcraft

    Eisenberg, Joseph D. | NTRS | 1990
    projected year 2000 convertible technology limited to present gas generator technology. Propulsion systems for utilization on aircraft needing ...
    Keywords: Aircraft Propulsion And Power

      The selection of convertible engines with current gas generator technology for high speed rotorcraft

      Eisenberg, Joseph D. | NTRS | 1990
      projected year 2000 convertible technology limited to present gas generator technology. Propulsion systems for utilization on aircraft needing ...
      Keywords: Aircraft Propulsion And Power

    The ROTONET prediction system and initial comparisons with far-field acoustics measurements for the XV-15 tilt-rotor aircraft

    Golub, Robert A. / Weir, Donald S. | NTRS | 1990
    ROTONET System. A joint NASA/Bell Helicopter Textron Incorporated test of an XV-15 tilt-rotor aircraft is one of several flight test which has ...

    Theoretical and Experimental Studies on Unsteady Rotor-Fuselage Interactional Aerodynamics

    Gasser, D. / Bettschart, N. / Drouin, B. et al. | British Library Conference Proceedings
    Keywords: vertical lift aircraft design , aircraft design

    The MDA/BAe/GEAE/RR ASTOVL/CTOL Technology Demonstrator Team

    Martens, R. / American Helicopter Society | British Library Conference Proceedings
    Keywords: vertical lift aircraft design , aircraft design

    The Impact of Integrated Product Development on the Helicopter Design Process

    House, T. L. / American Helicopter Society | British Library Conference Proceedings
    Keywords: vertical lift aircraft design , aircraft design

    The Direct Lift ASTOVL Aircraft

    Brower, D. / American Helicopter Society | British Library Conference Proceedings
    Keywords: vertical lift aircraft design , aircraft design

    The Design, Development and Testing of a Turbine Powered Simulator for Hot Gas Ingestion Testing

    Xu, Liping / Ford, Paul / Curtis, Peter | SAE Technical Papers | 2005
    This paper describes the problem of Hot Gas Ingestion (HGI) for vertical landing aircraft, and how it is measured and understood during ...
    Keywords: Aircraft

    The Autonomous Scout Rotorcraft Testbed (ASRT), A US Army IPPD Pilot Project

    Gordon, M. A. / Schrage, D. P. / Kuck, K. et al. | British Library Conference Proceedings
    Keywords: vertical lift aircraft design , aircraft design

    Technology Needs for Future US Navy/Marine Corps Heavy Lift VTOL Aircraft

    Troutman, S. P. / AHS International | British Library Conference Proceedings | 2006
    Keywords: Vertical lift aircraft , Aircraft design

    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

    Supplement to Conference Proceedings No. 22 Pre-Print

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