Correlation of transition Reynolds number with aerodynamic noise levels in a wind tunnel at Mach numbers 2.0-3.0
- 1 December 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (12) , 1670-1671
- https://doi.org/10.2514/3.7045
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Transition Reynolds number comparisons in several major transonic tunnelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974