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    Dynamic Calibration of the NASA Ames Rotor Test Apparatus Steady/Dynamic Rotor Balance (1996)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The NASA Ames Rotor Test Apparatus was modified to include a Steady/Dynamic Rotor Balance. The dynamic calibration procedures and configurations are discussed. Random excitation was applied at the rotor hub, and vibratory force and moment responses were measured on the steady/dynamic rotor balance. Transfer functions were computed using the load cell data and the vibratory force and moment responses from the rotor balance. Calibration results showing the influence of frequency bandwidth, hub mass, rotor RPM, thrust preload, and dynamic loads through the stationary push rods are presented and discussed.
    Keywords: Aircraft Design, Testing and Performance
    Type: NASA-TM-110393 , A-961452 , NAS 1.15:110393
    Format: application/pdf
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