Rotation Influence on Heat Transfer at Supersonic Flow Around a Blunted Body
Author:
Affiliation:
1. National Research Tomsk State University, 634050 Tomsk, Russia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056282
Reference34 articles.
1. Investigation of a hypersonic viscous shock layer on rotating axisymmetric bodies in the presence of blowing
2. Heat and mass transfer in unsteady compressible axisymmetric stagnation point boundary layer flow over a rotating body
3. Influence of rotation of the body and exterior vorticity on the heat transfer near the stagnation point of a blunt body in a supersonic stream
4. Computation of flow past a rotating cylinder with an energy-dissipation model of turbulence
5. The Prediction of Axisymmetric Turbulent Swirling Boundary Layers
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