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 aerodynamic shape of the hypersonic forebody/inlet integrated vehicle is usually
designed according to the inviscid flow. However, due to the effect of air viscosity, there is a …

With the aim of integrating a ramjet or scramjet with an airframe, a novel inlet–airframe
integration methodology for the hypersonic waverider vehicle is proposed. For this newly …

A novel Bump-integrated three-dimensional internal waverider inlet (IWI) design method is
presented for high-speed inlet/forebody integration. The low-kinetic-energy (boundary layer) …

A wavecatcher type scramjet intake, that reduces the Mach number number from 4 to 1.552,
is used as the basis for a study of flow starting/unstarting as affected by freestream angles of …

I. Introduction n the high-speed aircraft design community, the waveriders are well accepted
as high performance configurations. Waverider is a hypersonic aircraft design which …

论述了国内外在高超声速三维内收缩式进气道研究方面的最新研究动态, 重点阐述了三维变截面
内乘波式进气道的研究进展. 介绍了常规矩形进口进气道与乘波体外形一体化相关研究 …

The osculating axisymmetric flows concept is an extension of the concept of the osculating
cones for designing waveriders which is also utilized to design the three-dimensional …

The novel flow pattern type of high-external compression internal conical of C+ integrated
with variable-geometry internal waverider inlet is investigated in this paper. Firstly, based on …

The design of an inward-turning high-speed three-dimensional streamline-traced intake is
presented from osculating axisymmetric theory. To satisfy the osculating intake design …