Axisymmetric Viscous Flow Past Very Slender Bodies of Revolution
- 1 June 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (6) , 667-679
- https://doi.org/10.2514/8.9581
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Creep stability of columns and platesJournal of the Mechanics and Physics of Solids, 1957
- The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1956
- A Note on the Laminar Boundary Layer on a Circular Cylinder in Axial Incompressible FlowJournal of the Aeronautical Sciences, 1954
- Skin-Friction and Heat-Transfer Characteristics of a Laminar Boundary Layer on a Cylinder in Axial Incompressible FlowJournal of the Aeronautical Sciences, 1951
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949