04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
EFFECTS OF SHOCK IMPINGEMENT LOCATION ON PANEL AEROELASTIC STABILITY IN MACH REFLECTION
Y. He¹, A. Shi¹; ¹Northwestern Polytechnical University, China
The aeroelastic stability and chaotic motions of a two-dimensional heated panel in Mach reflection are investigated through theoretical analysis, which reveals the impact of shock impingement location on the stability boundary and discloses the stability region of post-divergence flutter, providing insight into the aeroelastic behavior of heated panels in Mach reflection.