Relationship between temperature and velocity profiles in a turbulent boundary layer along a supersonic nozzle with heat transfer
- 1 November 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (11) , 2066-2069
- https://doi.org/10.2514/3.6051
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Effect of wall cooling on the mean structure of a turbulent boundary layer in low-speed gas flowInternational Journal of Heat and Mass Transfer, 1970
- Acceleration and cooling effects in laminar boundary layers - Subsonic, transonic, and supersonic speedsAIAA Journal, 1970
- Atomic and Molecular Scattering from Solids. II. Comparison of Classical Scattering Models in Relation to ExperimentThe Journal of Chemical Physics, 1969
- Preliminary results from an experimental investigation of nozzle wall boundary layer at Mach numbers ranging from 27 to 47Published by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Influence of Pressure History on Momentum Transfer in Rarefied Gas FlowsPhysics of Fluids, 1960