Numerical studies of flow patterns and fuel distribution of tandem-arranged multi jets in a hypersonic crossflow

Author:

Wang JialinORCID,Han Guilai

Funder

National Key Research and Development Program of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference49 articles.

1. Detonative propulsion [J];Wolanski;Proc. Combust. Inst.,2013

2. Flow and combustion mechanism of oblique detonation engines;Teng;Sci. Sin.-Phys. Mech. Astron.,2020

3. A numerical study on the instability of oblique detonation waves with a two-step induction–reaction kinetic model [J];Yang;Proc. Combust. Inst.,2019

4. Formation of stabilized oblique detonation waves in a combustor [J];Zhang;Combust. Flame,2021

5. Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner [J];Wang;Aerosp. Sci. Technol.,2021

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