Foreign-Gas Injection Into a Compressible Turbulent Boundary Layer on a Flat Plate
- 1 August 1961
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 28 (8) , 645-654
- https://doi.org/10.2514/8.9118
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- On the Continuity of the Schmidt Number at the Interface Between the Laminar Sublayer and the Outer Turbulent RegionJournal of the Aerospace Sciences, 1959