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

121–140 of 160 hits
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    Flight Path Management and Configuration Control Methodology to Reduce Helicopter Blade-Vortex Interaction (BVI) Noise

    Gopalan, G. / Schmitz, F. / Sim, B. W.-C. et al. | British Library Conference Proceedings | 2000
    Keywords: vertical lift aircraft design , aircraft design

    A History of Individual Flying Platforms

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

    Analysis for the Application of Hybrid Laminar Flow Control to a Long-Range Subsonic Transport Aircraft

    Bartlett, D. W. / McCullers, L. A. / Arcara, P. C. | SAE Technical Papers | 1991
    aircraft are presented. The study was performed using the Flight Optimization System (FLOPS), a rapid and flexible conceptual design and analysis ...
    Keywords: Aircraft , Design processes , Aircraft tails

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

    Barrie, R. / Howell, H. / Labows, S. et al. | British Library Conference Proceedings | 2000
    Keywords: 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
    Keywords: 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
    Keywords: 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 ...
    Keywords: Aircraft , Design processes

    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

    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

    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 ...

    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 ...
    Keywords: Vertical take-off and landing (VTOL) , Aircraft , Design processes

    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 ...
    Keywords: 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 ...
    Keywords: 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
    Keywords: 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 ...
    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

    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 ...
    Keywords: Aircraft