Fully developed turbulent supersonic flow in a rectangular channel.
- 1 August 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (8) , 1331-1336
- https://doi.org/10.2514/3.3673
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Electrical conductivity measurements in a Faraday acceleratorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Loss Mechanisms of a Low Temperature Plasma AcceleratorARS Journal, 1962
- The Analogy Between Fluid Friction and Heat TransferTransactions of the American Society of Mechanical Engineers, 1939