Calculation of the boundary layer arising in flow about a cone under an angle of attack
- 1 January 1966
- journal article
- Published by Elsevier in USSR Computational Mathematics and Mathematical Physics
- Vol. 6 (2), 149-161
- https://doi.org/10.1016/0041-5553(66)90062-0
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Laminar boundary-layer development on yawed coneAIAA Journal, 1964
- AN INTEGRAL METHOD FOR CALCULATION OF SUPERSONIC LAMINAR BOUNDARY LAYER WITH HEAT TRANSFER ON YAWED CONEAIAA Journal, 1963
- Three-Dimensional Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1953