Wind Tunnel Pressure Probes: New Calibrations for New Geometries and Flow Environments
- 1 October 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (10), 1263-1264
- https://doi.org/10.2514/3.60536
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Viscous interaction effects on a static pressure probe at m equals 6AIAA Journal, 1963
- Hypersonic Viscous Flow Over Slender ConesJournal of the Aerospace Sciences, 1959