Synonyme wurden verwendet für: aircraft conference design lift
Suche ohne Synonyme: title: Vertical lift aircraft design conference

121–140 von 160 Ergebnissen
|

    Application of Adjoint Optimization Method to Multi-Element Rotorcraft Airfoils

    Chaffin, M. S. / American Helecopter Society International | British Library Conference Proceedings | 2000
    Schlagwörter: vertical lift aircraft design , aircraft design

    A History of Individual Flying Platforms

    Schroeder, J. A. / American Helecopter Society International | British Library Conference Proceedings | 2000
    Schlagwörter: vertical lift aircraft design , aircraft design

    A Low-Cost, High-Performance VTOL for the General Aviation Marketplace

    Barrie, R. / Howell, H. / Labows, S. et al. | British Library Conference Proceedings | 2000
    Schlagwörter: vertical lift aircraft design , aircraft design

    Linking a Solid-Modeling Capability with a Conceptual Rotorcraft Sizing Code

    Preston, J. R. / Peyran, R. J. / American Helecopter Society International | British Library Conference Proceedings | 2000
    Schlagwörter: vertical lift aircraft design , aircraft design

    Problem Definition for the Joint Transport Rotorcraft

    Schrage, D. P. / Brunson, K. / Grinsell, C. et al. | British Library Conference Proceedings | 2000
    Schlagwörter: vertical lift aircraft design , aircraft design

    SoloTrek™ XFV™ (Exo-Skeletor Flying Vehicle) -- An Inside Look

    Moshier, M. W. / Bulaga, R. W. / American Helecopter Society International | British Library Conference Proceedings | 2000
    Schlagwörter: vertical lift aircraft design , aircraft design

    SAE Aero Design '92

    Kaercher, Brandon W. | SAE Technical Papers | 1992
    Cedarville College participating in the SAE Aero Design Competition.The Cedarville entry is a high wing tail dragging monoplane. It uses a narrow ...
    Schlagwörter: Aircraft , Design processes

    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 ...
    Schlagwörter: 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 ...
    Schlagwörter: Aircraft Design, Testing And Performance

    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 ...
    Schlagwörter: Aircraft

    A Comparative Study of a Multi-Gas Generator Fan to a Turbofan Engine on a Vertical Takeoff and Landing Personal Air Vehicle

    Ahn, Byung Ho / Mavris, Dimitri N. / Lim, Dongwook | SAE Technical Papers | 2006
    to address the fundamental technical challenge in designing a VTOL aircraft: the significant mismatch between the power requirements at lift ...
    Schlagwörter: Vertical take-off and landing (VTOL) , Aircraft , Design processes

    Evaluation of Flying Qualities and Guidance Displays for an Advanced Tilt-Wing STOL Transport Aircraft in Final Approach and Landing

    Frost, Chad R. / Franklin, James A. / Hardy, Gordon H. | NTRS | 2002
    -wing Short Take-Off and Landing (STOL) transport aircraft during final approach and landing. The experiment was conducted to assess the design ...

    Influence of Alternative Engine Concepts on LCTR2 Sizing and Mission Profile

    Acree, C. W., Jr. / Snyder, Christopher A. | NTRS | 2012
    The Large Civil Tiltrotor (LCTR) was developed as part of the NASA Heavy Lift Rotorcraft Systems Investigation in order to establish a ...
    Schlagwörter: Aircraft Design, Testing And Performance

    Coaxial Compound Helicopter for Confined Urban Operations

    Johnson, Wayne / Elmore, Joshua F. / Keen, Ernest B. et al. | NTRS | 2016
    off-load the rotors at high speed, and ducted fans under the rotor disk for propulsion. The baseline design is described, and the aircraft ...
    Schlagwörter: Aircraft Design, Testing And Performance

    Cost Analysis for Large Civil Transport Rotorcraft

    Coy, John J. | NTRS | 2006
    120 passengers. The lowest cost VTOL design is a large civil tilt rotor (LCTR) aircraft. With cost tech factors applied, the LCTR is ...

    AERODYNAMIC CHARACTERISTICS OF TWO ROTARY WING UAV DESIGNS

    Jones, Henry E. / Wong, Oliver D. / Noonan, Kevin W. et al. | NTRS | 2006
    and an introduction to the test articles, and instrumentation. Sample data in the form of a parametric study of fixed system lift and drag ...

    Methodology for estimating helicopter performance and weights using limited data

    Baserga, Claudio / Ingalls, Charles / Lee, Henry et al. | NTRS | 1990
    Schlagwörter: Aircraft Design, Testing And Performance

    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 ...
    Schlagwörter: 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 ...
      Schlagwörter: Aircraft Propulsion And Power

    Experimental investigation of wingtip aerodynamic loading

    Van Aken, Johannes M. | NTRS | 1990
    wingtip sweep on the wingtip lift curve slope, drag polar, and pitching moment behavior is discussed. The obtained wingtip data was used to define ...

    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 ...
    Schlagwörter: Aircraft