Development of an Interactive Hypersonic Flow Solver Framework for Aerothermodynamic Analysis

Author:

Subrahmanyam Prabhakar

Publisher

Informa UK Limited

Subject

Modeling and Simulation,General Computer Science

Reference8 articles.

1. Baldwin BS, Lomax H (1978). Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows. AIAA Paper 78-0257.

2. Cebeci T, Smith AMO (1968). “A Finite-Difference Solution to the Incompressible Turbulent Boundary Layer Equations by an Eddy Viscosity Concept,” InComputation of Turbulent Boundary Layers, Volume 1, pages 346–355. AFOSR-IFP-Stanford Conference, Stanford University.

3. Coakley TJ (1983). Turbulence Modeling Methods for the Compressible Navier-Stokes Equations. AIAA Paper 83-1693.

4. Mitcheltree RA, Gnoffo PA (1994). Wake Flow about a MESUR Mars Entry Vehicle. AIAA Paper No. 94-1958.

5. Park C (1985). On Convergence of Computation of Chemically Reacting Flows. AIAA Paper No. 85-0247.

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