Performance Analysis of a Mach 12 Scramjet at Off-Design Conditions
Author:
Affiliation:
1. Centre for Hypersonics, University of Queensland, Brisbane, Queensland 4072, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34563
Reference7 articles.
1. A Review of Fuel Pre-injection in Supersonic, Chemically Reacting Flows
2. Application of Inlet Injection to a Three-Dimensional Scramjet at Mach 8
3. Control of Hypersonic Turbulent Skin Friction by Boundary- Layer Combustion of Hydrogen
4. Shock-Tunnel Experiments with a Mach 12 Rectangular-to-Elliptical Shape-Transition Scramjet at Offdesign Conditions
5. Scramjets
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