Design of Static Pressure Probes for Improved Free-Stream Characterization in Hypersonic Wind-Tunnels
Author:
Affiliation:
1. von Kármán Institute for Fluid Dynamics
2. Royal Observatory of Belgium
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-1410
Reference34 articles.
1. Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20
2. Viscous interaction effects on a static pressure probe at m equals 6
3. Lecture Series 86;Meier H. U.,1976
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