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Highly separated transonic flowsAttention is given to the wind tunnel, to photographic visualization of the flow, and to measurements by pressure probes, hot wire anemometry and laser anemometry. The simultaneous use of different means of measurement provided a good description of the phenomenon, and indicated the existence of shocks and their stability, as well as the existence of the bubble, its dimensions, and in particular, the reattachment of its front. The results show that the bursting (or transition) of the bubble front is produced at an unstable position and creates a point of turbulent intensity which diffuses over the entire height of the flow.
Document ID
19810013490
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Farcy, A.
(NASA Headquarters Washington, DC United States)
Mercier, V.
(NASA Headquarters Washington, DC United States)
Leblanc, R.
(NASA Headquarters Washington, DC United States)
Goethals, R.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
NT80-18
NASA-TM-75874
Report Number: NT80-18
Report Number: NASA-TM-75874
Meeting Information
Meeting: Colloq. Aerodyn. Appl.
Location: Lille
Country: France
Start Date: November 13, 1979
End Date: November 15, 1979
Accession Number
81N22020
Funding Number(s)
CONTRACT_GRANT: NASW-3198
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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