Hot-Film Probe Technique for Monitoring Shock-Wave Oscillations
- 1 December 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 16 (12) , 871-875
- https://doi.org/10.2514/3.58615
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Some features of the unsteady pressure field in transonic airfoil buffetingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Measured Three-Dimensional Effects in Transonic Airfoil TestingAIAA Journal, 1975
- Surface pressure and wake flow fluctuations in a supercritical airfoil flowfieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975