Airbreathing aero-engines are regarded as excellent propulsion devices from ground takeoff
to hypersonic flight, and require control systems to ensure their efficient and safe operation …

A spiked blunt body flying at hypersonic speed could result in significant thermal interactions
between the external flowfield and the internal structure, which have not received enough …

The turbine based combined cycle engine has become the most promising hypersonic
airbreathing propulsion system for its superiority of ground self-starting, wide flight envelop …

Mechanical cutting assisted by high-pressure jet is a common and efficient drilling method in
the exploration of hot dry rock (HDR). The drilling efficiency can be further improved with an …

In this paper, the mode transition process of an over-under exhaust system for a turbine
based combined cycle (TBCC) is investigated experimentally. The method of characteristics …

The present study focuses on the unsteady mode transition process of an over-under TBCC
exhaust system. The method of characteristics is applied to design the over-under TBCC …

Serpentine nozzle can effectively suppress the infrared radiation signatures of the aero-
engine exhaust system. However, it experiences the remarkable fluid-structure interaction …

In this paper, a hybrid Lattice Boltzmann Flux Solver (LBFS) with an improved switch
function is proposed for simulation of integrated hypersonic fluid-thermal-structural …

为实现三维并联式TBCC 排气系统的设计, 利用基于二维最大推力理论的密切法设计了圆转矩变
截面非对称冲压发动机喷管, 并在冲压发动机喷管上壁面为三维曲面的条件下 …

The present study focuses on the design and performance analysis of an exhaust system for
an over-under turbine based combined cycle (TBCC) operating at Mach 0–6. The …