Asymptotic boundary-layer over a slender body of revolution in axial compressible flow
- 1 May 1965
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (5) , 809-816
- https://doi.org/10.2514/3.3000
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- On thick boundary layers over slender bodies with some effects of heat transfer, mass transfer and pressure gradientInternational Journal of Heat and Mass Transfer, 1962
- Axisymmetric Viscous Flow Past Very Slender Bodies of RevolutionJournal of the Aerospace Sciences, 1962
- The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1956
- The axisymmetric boundary layer on a long thin cylinderProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1955
- Skin-Friction and Heat-Transfer Characteristics of a Laminar Boundary Layer on a Cylinder in Axial Incompressible FlowJournal of the Aeronautical Sciences, 1951