Three-dimensional flow analysis in a rocket engine coolant channel of high depth/width ratio
Author:
Affiliation:
1. MBB GmbH, Munich, Federal Republic of Germany
2. Advanced Scientific Computing GmbH, Holzkirchen, Federal Republic of Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-2183
Reference16 articles.
1. Numerical Computation of Turbulent Flow in a Square-Sectioned 180 Deg Bend
2. Turbulent Boundary-Layer Development Around a Square-Sectioned U-Bend: Measurements and Computation
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