Synonyme wurden verwendet für: HUBSCHRAUBER
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1–19 von 19 Ergebnissen
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    An aeroelastic analysis methodology for bearingless main rotor helicopters

    Gandhi, F. / Chopra, I. | Tema Archiv | 1998
    Schlagwörter: Hubschrauber

    A Physics-Based Approach to Trim Optimization of an Articulated Slowed-Rotor Compound Helicopter in High-Speed Flight

    Reddinger, J. / Gandhi, F. / American Helicopter Society | British Library Conference Proceedings | 2014
    Schlagwörter: Helicopters

    CFD Analysis of High-Lift Devices on the SC-1094R8 Airfoil

    Bae, E.S. / Gandhi, F. / AHS International | British Library Conference Proceedings | 2011
    Schlagwörter: Helicopters

    Design, Development, and Hover Testing of a Helicopter Rotor Blade Chord Extension Morphing System

    Gandhi, F. / Hayden, E. / American Helicopter Society | British Library Conference Proceedings | 2014
    Schlagwörter: Helicopters

    DESIGN, FABRICATION AND BENCHTOP TESTING OF A HELICOPTER ROTOR BLADE SECTION WITH WARP-INDUCED SPANWISE CAMBER VARIATION

    Mistry, M. / Gandhi, F. / American Helicopter Society | British Library Conference Proceedings | 2013
    Schlagwörter: Helicopters

    Extendable Chord Rotors for Helicopter Envelope Expansion and Performance Improvement

    Gandhi, F. / Khoshlahjeh, M. / Webster, S. et al. | British Library Conference Proceedings | 2011
    Schlagwörter: Helicopters

    HELICOPTER ROTOR PERFORMANCE IMPROVEMENT WITH RPM VARIATION AND CHORD EXTENSION MORPHING

    Khoshlahjeh, M. / Gandhi, F. / American Helicopter Society | British Library Conference Proceedings | 2013
    Schlagwörter: Helicopters

    Helicopter vibration reduction through cyclic variations in rotor blade root stiffness

    Anusonti-Inthra, P. / Gandhi, F. | Tema Archiv | 2000
    Schlagwörter: Hubschrauber

    Helicopter vibration reduction using discrete controllable-stiffness devices at the rotor hub

    Gandhi, F. / Anusonti-Inthra, P. | Tema Archiv | 2001
    Schlagwörter: Hubschrauber

    Helicopter vibration reduction using fixed-system auxiliary moments

    Gandhi, F. / Sekula, M.K. | Tema Archiv | 2004
    Schlagwörter: Hubschrauber

    Hover Performance Improvement with Warp-Induced Spanwise Camber Variation

    Mistry, M. / Gandhi, F. / Vertical Flight Technical Society | British Library Conference Proceedings | 2012
    Schlagwörter: Helicopters

    Influence of balanced rotor anisotropy on helicopter aeromechanical stability

    Gandhi, F. / Malovrh, B. | Tema Archiv | 1999
    Schlagwörter: Hubschrauber

    Reversible Airfoils for Stopped Rotors in High Speed Flight

    Niemiec, R. / Jacobellis, G. / Gandhi, F. et al. | British Library Conference Proceedings | 2014
    Schlagwörter: Helicopters

    ROTOR STALL ALLEVIATION WITH ACTIVE GURNEY FLAP

    Bae, E.S. / Gandhi, F. / American Helicopter Society | British Library Conference Proceedings | 2013
    Schlagwörter: Helicopters

    Upstream Active Gurney Flap for Rotorcraft Vibration Reduction

    Bae, E.S. / Gandhi, F. / Vertical Flight Technical Society | British Library Conference Proceedings | 2012
    Schlagwörter: Helicopters