Design of a wing shape for study of hypersonic crossflow transition in flight
- 31 December 1992
- journal article
- Published by Elsevier in Computing Systems in Engineering
- Vol. 3 (1-4) , 115-130
- https://doi.org/10.1016/0956-0521(92)90099-5
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Compressible laminar boundary layers with suction on swept and tapered wingsJournal of Aircraft, 1977
- A note on the relation between temporally-increasing and spatially-increasing disturbances in hydrodynamic stabilityJournal of Fluid Mechanics, 1962