Near-Body Measurements in Hypersonic Cylinder Flows in the T5 Reflected Shock Tunnel by Tunable Diode Laser Absorption Spectroscopy
Author:
Affiliation:
1. Stanford University
2. California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1705
Reference31 articles.
1. The X-51A Scramjet Engine Flight Demonstration Program
2. The DARPA/AF Falcon Program: The Hypersonic Technology Vehicle #2 (HTV-2) Flight Demonstration Phase
3. Hypersonic International Flight Research and Experimentation Technology Development and Flight Certification Strategy
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