The Basis of an Industry-standard Aerodynamic Computation and its Theoretical Basis with Inferences and Applications

Author:

Gao Z.

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference39 articles.

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2. Davis RT. Numerical solution of the hypersonic viscous shock-layer Eqs.[J] AIAA Jour. 1970,8(5):843-851.

3. Gao Z. Combined solution of both viscous boundary layer with its outer inviscid flow and viscous inner wake with its outer inviscid wake. S-T Report, Institute of Mechanics, Chinese Academy of Sciences, A detailed abstract refers to “Simplified Navier-Stokes Eqs. and combined solution of viscous boundary layer with its outer inviscid flow” Acta Mechanica Sinica, 1982, 6(6):606-611.(in Chinese).

4. Rudman S, Rubin SG. Hypersonic viscous flow over slender bodies with sharp leading edges[J]. 1968,6(10):1883-1889.

5. Lubard SC, Helliwell WS. Calculation of the flow on a cone at high angle of attack[J]. AIAA Jour. 1974,12(7):965-974.

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