Mixing and combustion characteristics in a scramjet combustor with different distances between cavity and backward-facing step
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference49 articles.
1. Solid fuel ramjet combustor design;Krishnan;Prog Aerosp Sci,1998
2. Hypersonic airbreathing propulsion;Heiser,1994
3. A review of Backward-Facing Step (BFS) flow mechanisms, heat transfer and control;Chen;Therm Sci Eng Prog,2018
4. Cavity flame-holders for ignition and flame stabilization in scramjets: An overview;Ben-Yakar;J Propuls Power,2001
5. Space flight safety: Experiments and supercomputing;Smirnov;Acta Astronaut,2019
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