Shock-wave boundary-layer interaction study on a compression corner using pressure-sensitive paint

Shock-wave boundary-layer interaction study on a compression corner using pressure-sensitive paint

  1. Shock-wave boundary-layer interaction study on a compression corner using pressure-sensitive paint”,International Journal of Aerospace Innovations, Volume 4, Issue 1-2,1 March 2012, Pages 29- 40


Last updated on : 13-10-2017 06:44:21pm