Effects of Cooling on Boundary-Layer Transition on a Hemisphere in Simulated Hypersonic Flow

1962 ◽  
Vol 29 (12) ◽  
pp. 1454-1461 ◽  
Author(s):  
ROGER DUNLAP ◽  
A. M. KUETHE
Keyword(s):  
Boundary Layer ◽  
Hypersonic Flow ◽  
Boundary Layer Transition ◽  
Layer Transition

Unusual boundary-layer transition results on cones in hypersonic flow.

AIAA Journal ◽  
1969 ◽  
Vol 7 (4) ◽  
pp. 660-664 ◽  
Author(s):  
GEORGE G. MATEER ◽  
HOWARD K. LARSON
Keyword(s):  
Boundary Layer ◽  
Hypersonic Flow ◽  
Boundary Layer Transition ◽  
Layer Transition

Boundary Layer Transition on a Generic Model of Control Flaps in Hypersonic Flow

2019 ◽  
Author(s):  
Madlen Leinemann ◽  
Rolf Radespiel ◽  
Federico Muñoz ◽  
Sebastien Esquieu ◽  
Gregory McKiernan ◽  
...  
Keyword(s):  
Boundary Layer ◽  
Hypersonic Flow ◽  
Boundary Layer Transition ◽  
Generic Model ◽  
Layer Transition

Simple Methods for Determining the Virtual Origin of Turbulent Boundary Layers in Hypersonic Flow on Sharp-Edged Flat Plates

1974 ◽  
Vol 41 (3) ◽  
pp. 551-553
Author(s):  
E. J. Hopkins
Keyword(s):  
Boundary Layer ◽  
Skin Friction ◽  
Hypersonic Flow ◽  
Boundary Layers ◽  
Turbulent Boundary Layers ◽  
Boundary Layer Transition ◽  
Simple Relationship ◽  
Flat Plates ◽  
Layer Transition ◽  
Virtual Origin

For hypersonic Mach numbers up to about 8, the virtual origin for turbulent skin-friction calculations is shown to be close to the beginning of boundary-layer transition. A simple relationship between the beginning and end of boundary-layer transition is presented.

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