Energies | |
Numerical Study on the Solid Fuel Rocket Scramjet Combustor with Cavity | |
Xiang Zhao1  Chaolong Li1  Binbin Chen1  Likun Ma1  Zhixun Xia1  | |
[1] Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China; | |
关键词: solid-fuel rocket scramjet (SFRSCRJ); cavity; supersonic combustion; combustor performance; particle combustion; | |
DOI : 10.3390/en12071235 | |
来源: DOAJ |
【 摘 要 】
Scramjet based on solid propellant is a good supplement for the power device of future hypersonic vehicles. A new scramjet combustor configuration using solid fuel, namely, the solid fuel rocket scramjet (SFRSCRJ) combustor is proposed. The numerical study was conducted to simulate a flight environment of Mach 6 at a 25 km altitude. Three-dimensional Reynolds-averaged Navier–Stokes equations coupled with shear stress transport (SST)
【 授权许可】
Unknown