The PARC Distinction: A Practical Flow Simulator
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[1] H. Lomax,et al. Thin-layer approximation and algebraic model for separated turbulent flows , 1978 .
[2] G. Harloff,et al. Hypersonic turbulent wall boundary layer computations , 1988 .
[3] G. Cooper,et al. A computational fluid dynamics evaluation of test cell recirculationeffects on high-bypass turbofan engine surface pressure distributions , 1986 .
[4] Antony Jameson,et al. A multigrid finite volume method for solving the Euler and Navier-Stokes equations for high speed flows , 1989 .
[5] Thomas H. Pulliam,et al. Euler and Thin Layer Navier-Stokes Codes: ARC2D, ARC3D , 1984 .
[7] G. Cooper,et al. Analysis tool for application to ground testing of highly underexpanded nozzles , 1987 .
[8] R. F. Warming,et al. An implicit finite-difference algorithm for hyperbolic systems in conservation-law form. [application to Eulerian gasdynamic equations , 1976 .
[9] Frank G. Collins,et al. Upgrade of PARC2D to include real gas effects , 1990 .
[10] D. R. Reddy,et al. Three-dimensional viscous flow computations of high area ratio nozzles for hypersonic propulsion , 1991 .
[11] P. D. Thomas. Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles, theory , 1979 .
[12] G. Cooper,et al. CFD applications in an aerospace engine test facility , 1990 .
[13] W. Phares,et al. Application of Computational Fluid Dynamics to test facility and experiment design , 1986 .
[14] A. Jameson,et al. Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes , 1981 .
[15] J. Steger,et al. Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow , 1980 .