Diode Laser Sensor for Velocity Measurements in Hypervelocity Flows
Author:
Affiliation:
1. Stanford University, Stanford, California 94305-3032
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.7565
Reference11 articles.
1. The Tailored-Interface Hypersonic Shock Tunnel
2. Design and fabrication of a Mach 8 contoured nozzle for the LENS facility
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