Experimental investigation of unstart dynamics driven by subsonic spillage in a hypersonic scramjet intake at Mach 6
Author:
Affiliation:
1. Department of Aerospace Engineering, Indian Institute of Science, Bangalore 560012, Karnataka, India
2. Defence Research Development Laboratory, Hyderabad 500058, Telangana, India
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/1.5135096
Reference26 articles.
1. How Much Compression Should a Scramjet Inlet Do?
2. Hypersonic Airbreathing Propulsion
3. E. T. Curran and S. N. B. Murthy,Scramjet Propulsion(AIAA, 2001), Vol. 189, pp. 462–466.
4. Recent research progress on unstart mechanism, detection and control of hypersonic inlet
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