On cone frustum pressure gradient effects on transition
- 1 April 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 26 (4) , 500-502
- https://doi.org/10.2514/3.9924
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Nosetip bluntness effects on cone frustum boundary layer transition in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Effect of bluntness and angle of attack on boundary layer transition on cones and biconic configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Aerodynamic Calibration of the Aerospace Research Laboratories' M=6 High Reynolds Number FacilityPublished by Defense Technical Information Center (DTIC) ,1975
- Boundary-Layer Transition on Blunt Bodies with Highly Cooled Boundary LayersJournal of the Aerospace Sciences, 1960