Free-Jet Testing of a REST Scramjet at Off-Design Conditions
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2955
Reference7 articles.
1. Hyper-X Flight Engine Ground Testing for Flight Risk Reduction
2. Design of Three-Dimensional Hypersonic Inlets with Rectangular-to-Elliptical Shape Transition
3. Experimental Testing of a Hypersonic Inlet with Rectangular-to-Elliptical Shape Transition
4. Mach 4 Performance of Hypersonic Inlet with Rectangular-to-Elliptical Shape Transition
5. Computational investigation of the performance and back-pressure limits of a hypersonic inlet
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