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Theoretical and Experimental Studies of the Transonic Flow Field and Associated Boundary Conditions near a Longitudinally-Slotted Wind-Tunnel WallA theoretical examination of the slotted-wall flow field is conducted to determine the appropriate wall pressure drop (or boundary condition) equation. This analysis improves the understanding of the fluid physics of these types of flow fields and helps in evaluating the uncertainties and limitations existing in previous mathematical developments. It is shown that the resulting slotted-wall boundary condition contains contributions from the airfoil-induced streamline curvature and the non-linear, quadratic, slot crossflow in addition to an often neglected linear term which results from viscous shearing in the slot. Existing and newly acquired experimental data are examined in the light of this formulation and theoretical developments.
Document ID
19880006433
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Everhart, Joel Lee
(George Washington Univ., Washington, DC, United States)
Date Acquired
September 5, 2013
Publication Date
February 14, 1988
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-103381
NAS 1.15:103381
Report Number: NASA-TM-103381
Report Number: NAS 1.15:103381
Accession Number
88N15815
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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