The Effect of Surface Cooling on Laminar Boundary-Layer Stability
- 1 September 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (9), 635-636
- https://doi.org/10.2514/8.2057
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Effects of Pressure Gradient on Stability and Skin Friction in Laminar Boundary Layers in Compressible FluidsJournal 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
- Linearized Treatment of Supersonic Flow Through DuctsJournal of the Aeronautical Sciences, 1949