The investigation of a compressible laminar boundary layer past an elliptical cone

Author:

Vetlutsky V.N.,Ganimedov V.L.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference20 articles.

1. Calculation of the boundary layer arising in the flow around a cone at an angle of attack;Vvedenskaya;USSR Comput. Math. and Math. Phys.,1966

2. Calculation of the laminar boundary layer on pointed elliptical cones in a supersonic flow at incidences less limiting one;Bashkin;Trudy TsAGI. vyp.,1970

3. Laminar boundary layer in a compressible gas at a conical external flow;Bashkin;Trudy TsAGI, vyp.,1963

4. Investigation of heat transfer around sharp elliptical cones in a supersonic flow at large incidences;Bashkin;Izv. AN SSSR, MZhG,1969

5. On numerical solution of the problem on the boundary layer on an elliptical cone;Vetlutsky;Čisl. Metody Mekh. Splosnol Sredy,1977

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Investigation of a turbulent boundary layer on a hypersonic aircraft model;Journal of Applied Mechanics and Technical Physics;1999-01

2. Receptivity of the Mach-4 boundary layer on an elliptic cone to laser-generated localized freestream perturbations;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12

3. Compressible laminar boundary layer on a delta wing with attached shock wave;Journal of Applied Mechanics and Technical Physics;1986

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