Supersonic Combustion of a Scramjet Engine Using Hydrogen Fuel in Shock Tunnel
Author:
Affiliation:
1. Vikram Sarabhai Space Centre, Thiruvananthapuram 695 022, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056761
Reference51 articles.
1. Secondary injection of gases into a supersonic flow
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5. Mixing and Penetration Studies of Sonic Jets in a Mach 2 Freestream
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