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A parametric experimental study of the slotted-wall boundary conditionAn experimental study of slotted upper and lower walls in a two dimensional transonic wind tunnel with solid sidewalls is reported. Results are presented for several slot spacings and slot openness ratios. The experimental data were pressure measurements which were made on an airfoil model and on a sidewall near one of the slotted walls. The slotted-wall boundary condition coefficient, which related the pressure and streamline curvature near the wall, was determined from the wall pressure measurements. The measured wall-induced interference was correlated with the experimental values for the boundary condition coefficient. This correlation was compared with theory.
Document ID
19790011819
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Everhart, J. L.
(NASA Langley Research Center Hampton, VA, United States)
Barnwell, R. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: Advanced Technol. Airfoil Res., Vol. 1, Pt. 2
Subject Category
Aerodynamics
Accession Number
79N19990
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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