First-Order Slip Effects on the Compressible Laminar Boundary Layer Over a Slender Body of Revolution in Axial Flow
- 1 June 1961
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 28 (6) , 508-510
- https://doi.org/10.2514/8.9057
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- On Heat Transfer in Slip FlowJournal of the Aerospace Sciences, 1958
- The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1956