The boundary layer transition at supersonic velocities-Reference-Cited by-同舟云学术

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The boundary layer transition at supersonic velocities

Published:2014 Issue:2 Volume:78 Page:114-120
ISSN:0021-8928
Container-title:Journal of Applied Mathematics and Mechanics
language:en
Short-container-title:Journal of Applied Mathematics and Mechanics

Author:

Lebiga V.A.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials,Modelling and Simulation

Reference16 articles.

1. A program for transition research;Reshotko;AIAA Journal.,1975

2. Radiated aerodynamic noise effect on boundary layer transition in supersonic and hypersonic wind tunnels;Pate;AIAA Journal.,1969

3. Boundary-layer transition on supersonic cones in an aeroballistic range;Potter;AIAA Journal.,1975

4. Experimental investigation of boundary-layer transition at supersonic velocities;Struminskii;Fluid Dynamics,1972

5. Influence of the unit Reynolds number on transition in a supersonic boundary layer;Kharitonov;Fluid Dynamics,1974

Cited by 1 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. Laminar–turbulent transition reversal on blunt ogive body of revolution at hypersonic speeds;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-08-10

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