Enhancing the mixing characteristics of multi-hydrogen jets in scramjet engines through the implementation of fuel injection strategies and vortex generator positioning

Mixing and Combustion Studies Using Cavity-Based Flameholders in a Supersonic Flow

Mark Gruber, Jeffrey M. Donbar, C. D. Carter et al. · Journal of Propulsion and Power · 2004 · 373 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity

Hongbo Wang, Zhenguo Wang, Mingbo Sun et al. · Acta Astronautica · 2014 · 185 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +16

Combustion oscillations in a scramjet engine combustor with transverse fuel injection

Jeong‐Yeol Choi, Fuhua Ma, Vigor Yang · Proceedings of the Combustion Institute · 2005 · 151 citations

Engineering, Aerospace Engineering, Mechanical Engineering +16

Suppression of combustion mode transitions in a hydrogen-fueled scramjet combustor by a multi-channel gliding arc plasma

Rong Feng, Jiajian Zhu, Zhenguo Wang et al. · Combustion and Flame · 2021 · 148 citations

Engineering, Mechanical Engineering, Physics +16

The influence of the sinusoidal shock generator on the mixing rate of multi hydrogen jets at supersonic flow

Yicheng Li, M. Barzegar Gerdroodbary, Rasoul Moradi et al. · Aerospace Science and Technology · 2019 · 142 citations

Natural Sciences, Aerospace Engineering, Physics +10