Calculation of the boundary layer arising in flow about a cone under an angle of attack-Reference-Cited by-同舟云学术

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Calculation of the boundary layer arising in flow about a cone under an angle of attack

Published:1966-01 Issue:2 Volume:6 Page:149-161
ISSN:0041-5553
Container-title:USSR Computational Mathematics and Mathematical Physics
language:en
Short-container-title:USSR Computational Mathematics and Mathematical Physics

Author:

Vvedenskaya N.D.

Publisher

Elsevier BV

Subject

General Engineering

Reference6 articles.

1. Calculation of the three-dimensional laminar boundary layer on lines of spread;Avduyevskii;Izv. Akad. Nauk SSSR (Series Mekh. Mashin.),1962

2. Three-dimensional Flow about Smooth Bodies in an Ideal Gas;Babenko,1964

3. Three-dimensional laminar boundary-layer flow;Moore;J. aeronaut. Sci.,1953

4. Supersonic laminar boundary layer with heat transfer on jawed cone;Jen;Amer. Inst. Aeronaut. and Astron. J.,1963

5. Laminar boundary layer development on jawed cone;Jen;Amer. Inst. Aeronaut. and Astron. J.,1964

Cited by 8 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. Computing the compressible laminar boundary layer on a sharp body of bielliptic section;Journal of Applied Mechanics and Technical Physics;1991

2. Calculation of a laminar boundary layer on the leeward side of a triangular plate with supersonic leading edges;Journal of Applied Mechanics and Technical Physics;1989

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

4. The investigation of a compressible laminar boundary layer past an elliptical cone;Computers & Fluids;1982-01

5. Viscous flow over a cone at moderate incidence. Part 2. Supersonic boundary layer;Journal of Fluid Mechanics;1973-07-17

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