Analysis of Effects of Diffusion of a Foreign Gas Into the Laminar Boundary Layer of a Supersonic Flow of Air in a Tube
- 1 September 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 26 (9) , 602-603
- https://doi.org/10.2514/8.8215
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Preliminary Results of Measurement of Effects of Diffusion of Helium Into the Laminar Boundary Layer of a Supersonic Flow of Air in a Tube at Mach 5Journal of the Aerospace Sciences, 1959