NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Skin Friction Extracted from Surface Pressure in Incident Shock-Wave/Boundary-Layer InteractionHigh-resolution skin-friction fields are extracted from pressure-sensitive paint (PSP) data obtained in shock-wave/boundary-layer interaction (SWBLI). The method of extracting skin friction from surface pressure is described, including the fundamental relation between skin friction and surface pressure, the variational method, error analysis, and an approximate iterative method. The proposed method is based on a coupling relation between skin friction and surface pressure, where the boundary enstrophy flux is suitably modeled or approximated. This method is applied to unsteady PSP data obtained in incident SWBLIs at Mach 2.5 for different Reynolds numbers, revealing the skin-friction structures of the flows: particularly, the separation bubble induced by the incident shock wave. The extracted results are in good agreement with the data obtained by the surface-stress-sensitive film.
Document ID
20210013539
Acquisition Source
Glenn Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Tianshu Liu
(Western Michigan University Kalamazoo, Michigan, United States)
David M. Salazar
(Western Michigan University Kalamazoo, Michigan, United States)
Jim Crafton
(Innovative Scientific Solutions (United States) Dayton, Ohio, United States)
Nickolay Rogoshchenkov
(Innovative Scientific Solutions (United States) Dayton, Ohio, United States)
Colleen Ryan
(Innovative Scientific Solutions (United States) Dayton, Ohio, United States)
Mark R. Woike
(Glenn Research Center Cleveland, Ohio, United States)
David O. Davis
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
April 12, 2021
Publication Date
July 7, 2021
Publication Information
Publication: AIAA Journal
Publisher: American Institute of Aeronautics and Astronautics
Volume: 59
Issue: 10
Issue Publication Date: October 1, 2021
ISSN: 0001-1452
e-ISSN: 1533-385X
Subject Category
Instrumentation And Photography
Funding Number(s)
CONTRACT_GRANT: NNC14QA53P
CONTRACT_GRANT: 80NSSC19C0414
WBS: 109492.02.03.05.06.01
WBS: 109492.02.03.09.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
skin friction
shock wave
supersonic
surface measurement
instrumentation
boundary layer
No Preview Available