Analysis of turbulent skin friction in thick axisymmetric boundary layers.
- 1 June 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (6) , 821-825
- https://doi.org/10.2514/3.6838
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Rapid Engineering Calculation of Two-Dimensional Turbulent Skin FrictionPublished by Defense Technical Information Center (DTIC) ,1972
- A Simple Theory for the Two-Dimensional Compressible Turbulent Boundary LayerJournal of Basic Engineering, 1972
- An Analysis of Axisymmetric Turbulent Flow Past a Long CylinderJournal of Basic Engineering, 1972
- A New Integral Method for Analyzing the Turbulent Boundary Layer With Arbitrary Pressure GradientJournal of Basic Engineering, 1969
- The Law of the Wall in a Thick Axisymmetric Turbulent Boundary LayerJournal of Applied Mechanics, 1967