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 generic inlet is depicted based on a smooth Bézier curve, and the results and insights
from high-dimensional dynamic multi-objective optimization of small-sample high Mach …

Scramjet engines are one of the most economical and reliable high-speed airbreathing
propulsion technologies that can be used for low-cost satellite launchers and hypersonic …

Scramjet engines are one of the most promising hypersonic airbreathing propulsion
technologies for robust, efficient, and economical access to space. Multi-objective design …

To investigate the potential benefits of hydrogen fuel injection in a three-dimensional
scramjet inlet, flow through a Mach 12 rectangular-to-elliptical shape transitioning scramjet …

HYPERSONIC air-breathing flight will enable rapid transport as well as affordable access to
space (see, eg,[1]). Despite advances in high-speed propulsion analysis, adequate …

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 …

Flow separation due to shock wave/boundary layer interaction is dominated in blade
passage with supersonic relative incoming flow, which always accompanies aerodynamic …

This paper proposes a new design method employed for a practical integration of multistage
compression osculating cones waverider and Busemann inlet. The singularity based on …

To make a compromise between compression efficiency and aerodynamic performance, a
novel multistage optimization approach is proposed to improve the design of the shape …