Predicting distributed roughness induced transition with a four-equation laminar kinetic energy transition model

Author:

Liu Zaijie,Zhao Yatian,Chen Shusheng,Yan Chao,Cai Fangjie

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference61 articles.

1. Hypersonic and High-Temperature Gas Dynamics;Anderson,1989

2. Linear stability theory and the problem of supersonic boundary-layer transition;Mack;AIAA J.,1975

3. Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels;Pate;AIAA J.,1969

4. Laminar boundary layer stability experiments on a cone at Mach 8. IV – On unit Reynolds number and environmental effects;Stetson,1986

5. Laminar boundary layer stability experiments on a cone at Mach 8. V – Tests with a cooled model;Stetson,1989

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