A THREE-DIMENSIONAL INCOMPRESSIBLE PLOW SIMULATION METHOD AND ITS APPLICATION TO THE SPACE SHUTTLE MAIN ENGINE - Part I - Laminar Flow
Author:
Affiliation:
1. ROCKETDYNE, ROCKWELL INTERNATIONA, CANOGA PARK, CA
2. NASA AMES RESEARCH CENTER, MOFFETT FIELD, CA
3. ROCKETDYNE, ROCKWELL INTERNATIONAL, CANOGA PARK, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-175
Reference10 articles.
1. lHUng,C.M andKodulla,W. `ATime-SplitFinite-DifferenceAlgorithmforThree-DimensionalFlow-Field simulation', AIAAPaper 83-1957.
2. 8Pulliam,T.E and Steger,J. L.`ImplicitFmite-DifferenceSimulations of Three-Dimensional Compressible flow', Vol.18,No. 2,1980, pp159-167.
3. Numerical Calculation of Time-Dependent Viscous Incompressible Flow of Fluid with Free Surface
4. Implicit Finite-Difference Procedures for the Computation of Vortex Wakes
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