Three-dimensional laminar boundary-layer transition on a sharp 8 degcone at Mach 10
- 1 May 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (5) , 852-856
- https://doi.org/10.2514/3.5777
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Flight test measurements of boundary-layer transition on a nonablating 22 deg coneJournal of Spacecraft and Rockets, 1970
- Effect of boundary-layer transition on vehicle dynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Boundary-layer transition on a 10 deg cone in hypersonic flows.AIAA Journal, 1965