NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
New diagnostic technique for the study of turbulent boundary-layer separationDescription of a diagnostic technique for determining the unsteady character of turbulent boundary-layer separation. The technique uses thin platinum films mounted flush with the model surface. Voltages from these films provide measurements related to the flow character above the film. For illustration, results obtained by this technique are presented for the interaction of a hypersonic shock wave and a turbulent boundary layer, with and without separation.
Document ID
19740063401
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Horstman, C. C.
(NASA Ames Research Center Experimental Fluid Dynamics Branch, Moffett Fields, Calif., United States)
Owen, F. K.
(United Aircraft Research Laboratories East Hartford, Conn., United States)
Date Acquired
August 7, 2013
Publication Date
October 1, 1974
Publication Information
Publication: AIAA Journal
Volume: 12
Subject Category
Fluid Mechanics
Accession Number
74A46151
Distribution Limits
Public
Copyright
Other

Available Downloads

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