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Computer simulation of a wind tunnel test section with discrete finite-length wall slotsA computer simulation of a slotted wind tunnel test section which includes a discrete, finite-length wall slot representation with plenum chamber constraints and accounts for the nonlinear effects of the dynamic pressure of the slot outflow jet and of the low energy of slot inflow air was developed. The simulation features were selected to be those appropriate for the intended subsequent use of the simulation in a wall interference assessment procedure using sparsely located wall pressure measurements. It is demonstrated that accounting for slot discreteness is important in interpreting wall pressure measured between slots, and that accounting for nonlinear slot flow effects produces significant changes in tunnel-induced velocity distributions and, in particular, produces a longitudinal component of tunnel-induced velocity due to model lift. A characteristic mode of tunnel flow interaction with constraints imposed by the plenum chamber and diffuser entrance is apparent in simulation results and is derived analytically through a simplified analysis.
Document ID
19860014135
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kemp, W. B., Jr.
(College of William and Mary Williamsburg, VA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1986
Publication Information
Publisher: NASA
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.26:3948
NASA-CR-3948
Report Number: NAS 1.26:3948
Report Number: NASA-CR-3948
Accession Number
86N23606
Funding Number(s)
CONTRACT_GRANT: NCC1-69
PROJECT: RTOP 505-60-21-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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