A new technique for the direct calculation of bluntbody flow fields
- 1 January 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (1) , 161-163
- https://doi.org/10.2514/3.2814
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- The Theory of Laminar Boundary Layers in Compressible FluidsPhysics Today, 1964
- A CRITICAL STUDY OF THE DIRECT BLUNT BODY INTEGRAL METHODPublished by Defense Technical Information Center (DTIC) ,1962
- On the PLK Method and the Supersonic Blunt-Body ProblemJournal of the Aerospace Sciences, 1962
- Eine einfache Abschätzung für GrenzschichtenArchive of Applied Mechanics, 1962
- An Approximate Solution of the Direct Supersonic Blunt-Body Problem for Arbitrary Axisymmetric ShapesJournal of the Aerospace Sciences, 1960