NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Three-dimensional separation for interaction of shock waves with turbulent boundary layersFor the interaction of shock waves with turbulent boundary layers, obtained experimental three-dimensional separation results and correlations with earlier two-dimensional and three-dimensional data are presented. It is shown that separation occurs much earlier for turbulent three-dimensional than for two-dimensional flow at hypersonic speeds.
Document ID
19740027814
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Goldberg, T. J.
(NASA Langley Research Center Hypersonic Vehicles Div., Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1973
Publication Information
Publication: AIAA Journal
Volume: 11
Subject Category
Aerodynamics
Accession Number
74A10564
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available