Validation of a Comprehensive Aeroelastic Analysis for Tiltrotor Aircraft

摘要

A comprehensive aeroelastic analysis that can predict the performance, vibratory loads and aeroelastic stability of composite- copter, conversion and airplane modes of operation are modeled. Predictions from this analysis for trim controls, Heli- copter, conversion and airplane modes of operation are modeled. Predictions from this analysis for trim controls, response, loads and aeroelastic stability correlate as well with test data as do predictions from other established analyses.