A summary is presented of research progress in the design and technology of hypersonic air
intakes and variable-geometry turbine based combined cycle (TBCC) intakes. Development …

The flow field in a hypersonic inlet model at a design point of M= 6 has been studied
experimentally. The focus of the current study is to present the time-resolved flow …

In this study, a design methodology is examined for an airframe–inlet integrated full-
waverider vehicle that can take advantage of the waverider's ideal precompression surface …

The parallel modular inlet is a common configuration in a strutjet engine of the rocket-based
combined-cycle hypersonic vehicle. To study the flow interaction between two adjacent …

With the aims of overcoming the limitations of the existing basic flow model derived from an
axisymmetric generating body and extending the aerodynamic design method of the …

介绍了曲锥前体/内转进气道一体化的设计方法, 针对进气道侧壁外扩角这一设计因素,
设计了具有不同捕获形状的两套一体化构型, 并完成了两套模型在马赫数Ma= 6.0, 0 …

飞行器前体/高超声速内转式进气道的一体化设计已经成为吸气式高超声速推进系统研究的一个
热点. 从气动设计角度分析了高超声速内转式进气道及其与飞行器前体的一体化设计方法 …

针对高超声速飞行器一体化设计方法现状的分析, 阐明了吸气式发动机与乘波体飞行器之间高效
的一体化对于高超声速飞行的重要作用, 并从理论, 原理, 设计方法3 方面进行介绍 …

The unstarted flow field in a hypersonic inlet model at a design point of Ma 6 is studied
experimentally. The time-resolved spatial flow characteristics of the separation shock …

Inward-turning external compression intake is one of the hybrid intakes that employs both
external and internal compression intakes principle. This intake is commonly developed for …