Numerical Study of the Combustion Field in Dual-cavity Scramjet Combustor-Reference-Cited by-同舟云学术

Numerical Study of the Combustion Field in Dual-cavity Scramjet Combustor

Published:2015 Issue: Volume:99 Page:313-319
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Lu Wang,Zhansen Qian,Liangjie Gao

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference8 articles.

1. P.J. Waltrup. Liquid Fueled Supersonic Combustion Ramjets: A Research Perspective of the Past, Present and Future. AIAA-86-0158.

2. C. Lada, K. Kontis . Fluidic Control of Cavity Configurations at Subsonic and Supersonic Speeds.AIAA2005-1293.

3. N. Zhuang, F.S. Alvi, C. Shih. Another Look at Supersonic Cavity Flows and Their Control. AIAA2005-2803.

4. X. Zhang, J.A. Edwards. Experimental Investigation of Supersonic Flow over Two Cavities in Tandem. AIAA Journal, 1992, 30(5): 1182-1190.

5. E. Hassan. Multi-fluid dynamics for supersonic jet-and-crossflows and liquid plug rupture, in aerospace engineering. Ann Arbor: University of Michigan, 2012.

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