Influence of Favorable Pressure Gradients on a Mach 5.0 Turbulent Boundary Layer
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
2011-01-01
Conference paper
Electronic Resource
English
INFLUENCE OF FAVORABLE PRESSURE GRADIENTS ON A MACH 5.0 TURBULENT BOUNDARY LAYER
British Library Conference Proceedings | 2011
|British Library Conference Proceedings | 2012
|Turbulent spot growth in favorable pressure gradients
AIAA | 1984
|