Dual-code solution procedure for efficient computing equilibrium hypersonic axisymmetric transitional/turbulent flows

Author:

Hejranfar Kazem,Esfahanian Vahid,Kamali-Moghadam Ramin

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. B.S. Baldwin, H. Lomax, Thin-layer approximation and algebraic model for separated turbulent flow, AIAA Paper 78-257, in: 16th Aerospace Sciences Meeting, Huntsville, Alabama, Jan. 1978.

2. An implicit factored scheme for the compressible Navier–Stokes equations;Beam;AIAA Journal,1978

3. Comparison of hypersonic experiments and PNS predictions: Part I: Aerothermodynamics;Bhutta;Journal of Spacecraft and Rockets,1990

4. Analysis of Turbulent Boundary Layers;Cebeci,1974

5. Some properties of boundary layer flow during the transition form laminar to turbulent motion;Dhawan;Journal of Fluid Mechanics,1958

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