Model of the Engine Exhaust System at Transonic Flight Speeds
- 1 July 1975
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 12 (7) , 428-433
- https://doi.org/10.2514/3.56995
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Turbulent boundary-layer separation due to a forward-facing stepPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Flight and wind tunnel investigation of the effects of Reynolds number on installed boattail drag at subsonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Turbulent boundary-layer separation in front of a forward-facing step.AIAA Journal, 1967