A vector-oriented finite difference scheme for calculating three-dimensional compressible laminar and turbulent boundary layers on practical wing configurations
Author:
Affiliation:
1. National Aerospace Laboratory, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1020
Reference5 articles.
1. x 26 0.112 2-D Laminar FACOM 230-75 CPU *
2. FACOM 230-75 CPU using the program in [17] Keller Box Scheme
3. x 26 x 41 FACOM 230-75 APU ** 3-D Laminar ( Cebeci [161 ) IBM
4. FACOM 230-75 APU
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3. Linear stability of three-dimensional boundary layers over axisymmetric bodies at incidence;AIAA Journal;1992-04
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