Measurement of Vehicle Stability Coefficients in Hypersonic Wind Tunnels
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-3690
Reference10 articles.
1. Three-component force balance for flows of millisecond duration
2. Determining aerodynamic coefficients from high speed video of a free-flying model in a shock tunnel
3. Measurement of free-flight dynamic stability derivatives of cones in a hypersonic gun tunnel
4. Hypersonic Free Flight Measurement Techniques
5. Free-flight tests of reentry capsule models in free-piston shock tunnel
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