Stability of Compressible Laminar Boundary Layer with Internal Heat Sources or Sinks
- 1 May 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (5), 329-336
- https://doi.org/10.2514/8.3345
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Calculation of the Stability of the Laminar Boundary Layer in a Compressible Fluid on a Flat Plate with Heat TransferJournal of the Aeronautical Sciences, 1952
- A Free-Flight Investigation of the Possibility of High Reynolds Number Supersonic Laminar Boundary LayersJournal of the Aeronautical Sciences, 1952
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949
- On the stability for three-dimensional disturbances of viscous fluid flow between parallel wallsProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1933