Keywords: Rotor balance, Rotor loads, Balance calibration, Dynamic response
Abstract: The NASA Ames Rotor Test Apparatus was recently modified to include a steady/dynamic rotor balance. The calibration procedures and data reduction process to obtain static and dynamic calibration coefficients are discussed. Verification of the dynamic calibration procedures and the data processing for the low frequency range was accomplished by means of a hub imbalance run. Representative results of the balance predictions for the hub imbalance forces and moments are provided.
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