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Mass flux similarity for slotted transonic-wind-tunnel wallsA discussion of the flow field measurements obtained in the vertical plane at several stations along the centerline of slots in two different longitudinally slotted wind tunnel walls is presented. The longitudinal and transverse components of the data are then transformed using the concept of flow similarity to demonstrate the applicability of the technique to the development of the viscous shear flow along and through a slotted wall of an airfoil tunnel. Results are presented showing the performance of the similarity transformations with variations in tunnel station, Mach number, and airfoil induced curvature of the tunnel free stream.
Document ID
19920000788
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Everhart, Joel L.
(NASA Langley Research Center Hampton, VA, United States)
Goradia, Suresh H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-4281
NAS 1.15:4281
L-16864
Report Number: NASA-TM-4281
Report Number: NAS 1.15:4281
Report Number: L-16864
Accession Number
92N10006
Funding Number(s)
PROJECT: RTOP 506-40-41-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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