AIAA Journal · 1981 · 20 citations · 9 references
EngineeringAerospace EngineeringMechanical EngineeringAerodynamicsComputational Fluid DynamicsFluid DynamicsComputational AerodynamicsTransonic AerodynamicsBody Shape AnalysisComputational Fluid Dynamics For Transonic FlowCylindrical CoordinatesThree-dimensional Computational Fluid DynamicsThree-dimensional Flow ModelingTransonic FlowTransonic Flow SimulationUnsteady Potential Flow
An analysis has been developed t o predict transonic potential flow about three-dimensional objects including inlet, duct and body geometries. Finite-differences and line relaxation are used t o solve the complete potential flow equation. The coordinate system is independent of body geometry and hence places n o restrictions on body shape. Cylindrical coordinates have been used for the computer code. The analysis has been programmed for the Control Data Corporation CYBER 203 vector computer with this programming oriented t o take advantage of the vector processing capabilities of the computer. Comparisons of c o m p ~ ~ t e d results with experimental measurements are presented to verify the analysis.
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Calculation of plane steady transonic flows
Earll M. Murman, Julian D. Cole · AIAA Journal · 1971 · 623 citations
Scan line methods for displaying parametrically defined surfaces
Jeffrey M. Lane, Loren Carpenter, Turner Whitted et al. · Communications of the ACM · 1980 · 194 citations
Multilevel Adaptive Computations in Fluid Dynamics
Achi Brandt · AIAA Journal · 1980 · 102 citations