【摘 要】
:
Stability and bifurcation of a nonlinear supersonic panel under aerothermal loads are analyzed numerically in the present study.In the structural model,von
【机 构】
:
School of Astronautics,Northwestern Polytechnical University,Xi\'an 710062,P.R. China
【出 处】
:
The 5th International Conference on Nonlinear Science and Co