Fundamental study of supersonic combustion in pure air flow with use of shock tunnel
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference7 articles.
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2. G. Smeets, C. Quenett, Shock tube investigation of H2 combustion in a high temperature supersonic air flow (Scramjet), Proceeding of IUTAM Symposium on Combustion in Supersonic Flows, Netherlands, 1997, pp. 173–178.
3. Temporally resolved, two-line fluorescence imaging of NO temperature in a transverse jet in a supersonic cross flow;McMillin;Applied Optics,1993
4. A. Ben-Yakar, M. Kamel, C. Morris, R.K. Hanson, Experimental investigation of H2 transverse jet combustion in hypervelocity flows, AIAA-Paper, 97-3019, 1997.
5. Comparison of supersonic combustion between impulse and vitiation-heated facilities;Boyce;Journal of Propulsion and Power,2000
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