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

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    Metrics for NASA Aeronautics Research Mission Directorate (ARMD) Strategic Thrust 3B Vertical Lift Strategic Direction

    Hochstetler, Ronald D. / Salvano, Dan / Gorton, Susan A. | NTRS | 2017
    Strategic Thrust Area 3B "Vertical Lift Strategic Direction." ...
    Keywords: Aircraft Design, Testing And Performance

    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

    Design and Performance of Lift-Offset Rotorcraft for Short-Haul Missions

    Johnson, Wayne / Moodie, Alex M. / Yeo, Hyeonsoo | NTRS | 2012
    The design and performance of compound helicopters utilizing lift-offset rotors are examined, in the context of short-haul, medium-size ...
    Keywords: Aircraft Design, Testing And Performance

    Preliminary design of a supersonic Short-Takeoff and Vertical-Landing (STOVL) fighter aircraft

    NTRS | 1990
    requirements. A supersonic fighter aircraft with a short takeoff and vertical landing capability using the lift plus lift/cruise engine concept seems a ...
    Keywords: Aircraft Design, Testing And Performance

    Performance, Loads and Stability of Heavy Lift Tiltrotors

    Acree, Cecil W., Jr. / Johnson, Wayne | NTRS | 2006
    Summaries of rotor performance are presented for a 124,000-lb Large Civil Tilt Rotor (LCTR) design, along with isolated-rotor and fully ...
    Keywords: Aircraft Stability And Control

    Designs and Technology Requirements for Civil Heavy Lift Rotorcraft

    Johnson, Wayne / Yamauchi, Gloria K. / Watts, Michael E. | NTRS | 2006
    manufacturing cost comparable to fixed-wing aircraft. Risk reduction plans were developed to provide the strategic direction to support a heavy-lift ...
    Keywords: Aircraft Design, Testing And Performance

    Impact of Airfoils on Aerodynamic Optimization of Heavy Lift Rotorcraft

    Acree, Cecil W., Jr. / Martin, Preston B. / Romander, Ethan A. | NTRS | 2006
    airfoils were designed for each aircraft, and their effects on performance analyzed by CAMRAD II. Airfoil design criteria are discussed for each ...
    Keywords: Aircraft Design, Testing And Performance

    Design criteria for integrated flight/propulsion control systems for STOVL fighter aircraft

    Franklin, James A. | NTRS | 1993
    As part of NASA's program to develop technology for short takeoff and vertical landing (STOVL) fighter aircraft, control system designs ...
    Keywords: Aircraft Stability And Control

    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

    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

    Large-Scale V/STOL Experimental Investigations of an Ejector-Lift Fighter and a Twin Tilt-Nacelle Transport

    Dudley, Michael R. | NTRS | 2016
    -mounted thrust augmenting ejector and a ventral deflecting jet nozzle for vertical lift. The Grumman Aircraft Company, the Navy, and NASA ...
    Keywords: Aircraft Design, Testing And Performance , Powered Lift

    Conceptual Design and Performance Analysis for a Large Civil Compound Helicopter

    Russell, Carl / Johnson, Wayne | NTRS | 2012
    A conceptual design study of a large civil compound helicopter is presented. The objective is to determine how a compound helicopter ...
    Keywords: Aircraft Design, Testing And Performance

    Supersonic flow computations for an ASTOVL aircraft configuration

    Ramakrishnan, S. V. / Szema, K. Y. / Chakravarthy, S. R. et al. | NTRS | 1990
    supersonic flow past an Advanced Short Take-Off and Vertical Landing (ASTOVL) aircraft configuration. Lift, drag and pitching moment values obtained ...

    Aerodynamic design of the Cal Poly Da Vinci Human-Powered Helicopter

    Larwood, Scott / Saiki, Neal | NTRS | 1990
    design performance is also explained. The propellers were tested in a wind tunnel and results are compared with theoretical data. Successful ...
    Keywords: Aircraft Design, Testing And Performance

    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 ...

    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

    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

    Converting a C-130 Hercules into a Compound Helicopter: A Conceptual Design Study

    Kottapalli, Anjaney P. / Harris, Franklin D. | NTRS | 2012
    Currently, the US Military and NASA are investigating the feasibility of a Vertical/Short Take Off and Landing (VSTOL) aircraft that can ...
    Keywords: Aircraft Design, Testing And Performance

    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

    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