UNIFORMLY VALID SECOND-ORDER SOLUTION FOR SUPERSONIC FLOW OVER CRUCIFORM SURFACES
Open Access
- 1 January 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (1) , 179-185
- https://doi.org/10.2514/3.1487
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Theoretical and Experimental Investigation of Second-Order Supersonic Wing-Body InterferenceJournal of the Aerospace Sciences, 1960
- General Theory of High Speed AerodynamicsPublished by Walter de Gruyter GmbH ,1954
- CX. The shock strength in supersonic “conical fields.”Journal of Computers in Education, 1949