IN ADDITION to the personal interest by these authors, super-sonic combustion (SC) and
supersonic combustion ramjets (SCRJ) are potentially very important for future launchers …

The turbulence–chemistry interaction model with finite-rate chemistry is a common model for
solving supersonic turbulent combustion and takes into consideration the interaction …

This paper reviews numerical simulations and modeling of high-speed combustion as it
pertains to scramjets. Simulation results were presented from various researchers that have …

This paper presents the effect of cavity-based injection in an axisymmetric supersonic
combustor using numerical investigation. An axisymmetric cavity-based angled and …

Supersonic combustion is a key issue in any future plan to develop supersonic combustion
(SC) ramjets (SCRJ) and rocket based combined cycles (RBCC) vehicles. Past experience …

These LES simulations show that by decreasing Sct from 0.7 to 0.6, the flame becomes
stable and once ignited it does not quench. Furthermore, the flame is more intense and no …

Mixing and combustion of supersonic reacting flows are currently under investigation for
scramjet engines. Experimental results at NASA-Langley RC with single-jet hydrogen …

Numerical simulations of the same test case have also been done to better understand
physics of supersonic reacting flows. These simulations have included the subgrid scale …

为了发展超声速湍流燃烧中化学反应源项的封闭方法, 更精确地模拟湍流燃烧相互作用,
引入两类化学反应有限速率模型: PaSR (Partially Stirred Reactor) 模型及其可压缩性修正模型 …

Mixing and combustion in supersonic reacting flows are currently under investigation for
new generation launchers and trans-atmospheric vehicles. Experimental results with …