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1–20 von 62 Ergebnissen
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    Preliminary results of the first static calibration of the RSRA helicopter active-isolator rotor balance system

    Acree, C. W., Jr. | NTRS | 1983
    Schlagwörter: Aircraft Design, Testing And Performance

    Preliminary report on in-flight measurement of rotor hub drag and lift using the RSRA

    Acree, C. W., Jr. | NTRS | 1985
    Schlagwörter: Aircraft Design, Testing And Performance

    Numerical analysis of the first static calibration of the RSRA helicopter active-isolator rotor balance system

    Acree, C. W., Jr. | NTRS | 1985
    Schlagwörter: Aircraft Design, Testing And Performance

    In-flight measurement of rotor hub drag using the RSRA - A feasibility demonstration

    Acree, C. W., Jr. / Kufeld, Robert M. | NTRS | 1985
    Schlagwörter: Aircraft Design, Testing And Performance

    Calculated performance, stability and maneuverability of high-speed tilting-prop-rotor aircraft

    Johnson, Wayne / Lau, Benton H. / Bowles, Jeffrey V. | NTRS | 1986
    Schlagwörter: Aircraft Design, Testing And Performance

    Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft

    Johnson, Wayne / Lau, Benton H. / Bowles, Jeffrey V. | NTRS | 1986
    Schlagwörter: Aircraft Design, Testing And Performance

    The effect of nonlinear elastomeric lag damper characteristics on helicopter rotor dynamics

    Felker, Fort F. / Lau, Benton H. / Mclaughlin, Stacey et al. | NTRS | 1987
    Schlagwörter: Aircraft Design, Testing And Performance

    Identification of XV-15 aeroelastic modes using frequency sweeps

    Acree, C. W., Jr. / Tischler, Mark B. | NTRS | 1989
    Schlagwörter: Aircraft Design, Testing And Performance

    Application of the joined wing to tiltrotor aircraft

    Wolkovitch, Julian / Wainfan, Barnaby / Ben-Harush, Yitzhak et al. | NTRS | 1989
    Schlagwörter: Aircraft Design, Testing And Performance

    Hub loads analysis of the SA349/2 helicopter

    Heffernan, Ruth M. / Yamauchi, Gloria K. / Gaubert, Michel et al. | NTRS | 1990
    Schlagwörter: Aircraft Design, Testing And Performance

    Aeroelastic loads and stability investigation of a full-scale hingeless rotor

    Peterson, Randall L. / Johnson, Wayne | NTRS | 1991
    Schlagwörter: Aircraft Design, Testing And Performance

    An improved CAMRAD model for aeroelastic stability analysis of the XV-15 with advanced technology blades

    Acree, C. W., Jr. | NTRS | 1993
    Schlagwörter: Aircraft Design, Testing And Performance

    Analysis of Advanced Rotorcraft Configurations

    Johnson, Wayne | NTRS | 2000
    Schlagwörter: Aircraft Design, Testing And Performance

    Effects of Rotor Design Variations on Tiltrotor Whirl-Mode Stability

    Acree, C. W., Jr. | NTRS | 2000
    Schlagwörter: Aircraft Design, Testing And Performance

    Rotor Design Options for Improving V-22 Whirl-Mode Stability

    Acree, C. W., Jr. / Price, George / Rutkowski, Michael | NTRS | 2001
    Schlagwörter: Aircraft Design, Testing And Performance

    Effects of Rotor Design Variations on Tiltrotor Whirl-Mode Stability

    Acree, C. W., Jr. / Rutkowski, Michael | NTRS | 2001
    Schlagwörter: Aircraft Design, Testing And Performance

    Influence of Wake Models on Calculated Tiltrotor Aerodynamics

    Johnson, Wayne | NTRS | 2001
    Schlagwörter: Aircraft Design, Testing And Performance

    Calculation of the Aerodynamic Behavior of the Tilt Rotor Aeroacoustic Model (TRAM) in the DNW

    Johnson, Wayne | NTRS | 2001
    Schlagwörter: Aircraft Design, Testing And Performance

    Airloads and Wake Geometry Calculations for an Isolated Tiltrotor Model in a Wind Tunnel

    Johnson, Wayne | NTRS | 2003
    Schlagwörter: Aircraft Design, Testing And Performance

    Effects of Blade Sweep on V-22 Whirl Flutter and Loads

    Acree, C. W., Jr. | NTRS | 2003
    Schlagwörter: Aircraft Design, Testing And Performance