Particle Image Velocimetry in Mach 3.5 and 4.5 Shock-Tunnel Flows
Author:
Affiliation:
1. French– German Research Institute of Saint-Louis, 68301 Saint-Louis, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1787
Reference13 articles.
1. Introduction
2. Application of particle image velocimetry to Mach 6 flows
3. A survey of particle image velocimetry applications in Langley aerospace facilities
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