Effect of Upstream Energy Deposition Rate on Flow Characteristics of a Scramjet Engine
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-5752-1_67
Reference11 articles.
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2. Devaraj MKK, Jutur P, Rao SM, Jagadeesh G, Anavardham GT (2021) Investigation of local unstart in a hypersonic scramjet intake at a mach number of 6. Aerosp Sci Technol 115:106789
3. Wagner JL, Yuceil KB, Valdivia A, Clemens NT, Dolling DS (2009) Experimental investigation of unstart in an inlet/isolator model in mach 5 flow. AIAA J 47(6):1528–1542
4. Falempin F, Wendling E, Goldfeld M, Starov A (2006) Experimental investigation of starting process for a variable geometry air inlet operating from Mach 2 to Mach 8. In: 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, p 4513
5. Teng J, Yuan H (2015) Variable geometry cowl sidewall for improving rectangular hypersonic inlet performance. Aerosp Sci Technol 42:128–135
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