Detonation-based propulsion has been an area of interest in the scientific community in
terms of detonative combustion providing higher efficiency. However, most detonation …

The shock-induced atomization and burning of liquid fuel droplets are paramount for
hypersonic propulsion and detonation-based combustion systems. The present work …

In this paper, aerobreakup in the stagnation region of high-Mach-number flow over a bluff
body is studied with experiments and computations. Water drops of diameter 0.51–2.30 mm …

In this paper, the interaction characteristics between the gaseous detonation and the water
droplet are numerically investigated, utilizing a modified compressible two-phase flow model …

In this paper, mathematical models and numerical algorithm are conducted for simulating
compressible two-phase multi-component reactive flows, coupling with the finite-rate-based …

To gain insight into shock–droplet interaction and detonation wave–droplet interaction in the
real physical environment, two solvers named interTwoPhaseLSCentralFoam and …

High-speed propulsion is a challenging and critical area of research. A major challenge with
high-speed propulsion is the limited time scales available to mix and combust the flow within …

Liquid droplet breakup and lifetime are critical parameters in the design and performance of
a liquid rocket engine. Previous studies have characterized the breakup mechanisms by …

利用VOF (流体体积法) 多相流模型和RNG (重整化群) k-ε 湍流模型, 通过数值模拟方法研究了
不同初始压力(20, 30, 40 kPa) 和当量比(0.8~ 1.2) 下, 爆震波对煤油液滴破碎 …

In this paper, we study the interaction of an H2-O2 detonation colliding with an RP-2 droplet.
The Kelvin-Helmholtz Rayleigh-Taylor (KHRT) model is one of the prevalent, semi-analytical …