Laminar Heat Transfer in Two-Dimensional Subsonic Effusors
- 1 June 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (6), 425-430
- https://doi.org/10.2514/8.3360
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- A Method for Analyzing the Heat Insulating Properties of the Laminar Compressible Boundary LayerJournal of the Aeronautical Sciences, 1954
- Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause SeparationJournal of the Aeronautical Sciences, 1953