03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
EXPERIMENTAL COMPARISON OF LIMIT CYCLE METHOD WITH PHASE RESONANCE AND PHASE SEPARATION METHODS FOR DETERMINING MODAL CHARACTERISTICS OF AIRCRAFT STRUCTURES
P.G. Karkle¹, G.V. Liseykin¹, M.A. Pronin¹; ¹TsAGI, Russia
IN THIS PAPER THE LIMIT CYCLES METHOD IS DESCRIBED AND EXPERIMENTAL COMPARISON OF LIMIT CYCLE METHOD WITH PHASE RESONANCE AND PHASE SEPARATION METHODS IS GIVEN.