The aeroelastic response of a plate with supersonic freestream flow on one side and a
shallow cavity on the other to turbulent pressure fluctuations is investigated computationally …

This study assesses the robustness and efficiency of the enriched piston theory approach for
modeling aeroelastic loads in the presence of impinging shocks. Both stationary and …

Balancing accurate and efficient estimation of aerothermodynamic loads is a significant
challenge for multidisciplinary modeling and analysis of high-speed vehicles. This study …

A novel parametric reduced-order model (ROM) is proposed for efficiently predicting
hypersonic unsteady aerodynamic responses under different flight conditions. The …

Turbulence, flow separation, and shock dynamics challenge the modeling and analysis of
high-speed aeroelastic behavior. Motivated by this, the importance of modeling the fidelity of …

Due to the maneuver and overload requirements of aircraft, it is inevitable that supersonic
fins experience high angles of attack (AOAs) and viscous effects at high altitudes. The local …

A surrogate-based modeling strategy is presented for robust and efficient prediction of
unsteady aeroelastic loads in the presence of shock-induced separation. Enriched piston …

For general hypersonic vehicles flying at high altitudes and Mach numbers, the appearance
of the large boundary layer displacement thickness can change the pressure distribution …

乘波体的高升阻比优势使其在高超声速飞行器设计中极具应用前景. 在实际工程应用中,
为了满足防热要求, 乘波体前缘必须进行钝化处理, 前缘钝化对乘波体气动性能会产生显著影响 …

The waverider has an extensive application prospect in the design of hypersonic vehicles
due to its excellent aerodynamic efficiency. However, it is known that the original cone …