Calculation of Compressible Turbulent Boundary Layers with Heat and Mass Transfer
- 1 June 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (6) , 1091-1097
- https://doi.org/10.2514/3.49920
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Behavior of turbulent flow near a porous wall with pressure gradientAIAA Journal, 1970
- SYNOPTIC: Calculation of Compressible Adiabatic Turbulent Boundary LayersAIAA Journal, 1970
- Laminar and Turbulent Incompressible Boundary Layers on Slender Bodies of Revolution in Axial FlowJournal of Basic Engineering, 1970
- A Finite-Difference Method for Calculating Compressible Laminar and Turbulent Boundary LayersJournal of Basic Engineering, 1970
- Solution of the Incompressible Turbulent Boundary-Layer Equations With Heat TransferJournal of Heat Transfer, 1970
- Direct measurement of skin friction on a porous flat plate with massinjection.AIAA Journal, 1967