It is difficult to rapidly solve fluid-thermo-structural coupling physical fields in modeling of
hypersonic vehicles. Particularly, their real-time simulation is more challenging due to the …

Rocket based combined cycle (RBCC) engine is regarded as one of the most efficient
propulsion systems for reusable space transportation vehicles and hypersonic cruise …

静气动弹性问题考虑弹性结构与定常气动力间的相互耦合作用, 对飞行器的性能和安全具有显著
的影响. 在现代飞行器设计阶段, 计算流体力学(CFD)/计算结构力学(CSD) 直接耦合方法是精确 …

To break the limitation of the conventional passive flutter and nonlinear aeroelastic
suppressions, a supersonic functionally graded material (FGM) plate featuring periodically …

A two-dimensional mixed compression scramjet inlet design is presented in this work. The
design is based on the static temperature and Mach number at the combustion chamber …

Reducing aeroelastic vibration of supersonic aircraft wings is very challenging because of
the limitation of efficiency, mass, space and especially the extreme high and variable …

RBCC engine commonly fulfills the ejector-to-ramjet mode transition at a Mach number far
below 4, and thus the divergent kerosene-fueled RBCC combustor will encounter tough …

Mode localization in the airflow direction can be observed in aeroelastic structures. On the
contrary, can the aeroelastic stability of the structure be enhanced if the geometric sizes and …

When the composite structure is subjected to high-power laser irradiation and high-speed
airflow, its ablation behavior presents significant localized characteristics and strong …

Aerodynamic interference occurs when biplane wings are placed close to each other.
Investigating aerodynamic interference on the transonic flutter characteristics of these wings …