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A wall interference assessment/correction systemThe Hackett method (a Wall Pressure Signature Method) was selected to be adapted for the 12 ft Wind Tunnel WIAC system. This method uses limited measurements of the static pressure at the wall, in conjunction with the solid wall boundary condition, to determine the strength and distribution of singularities representing the test article. The singularities are used in term for estimating wall interference at the model location. Hackett's method will have to be formulated for application to the unique geometry of the 12 ft tunnel. The WIAC code will be validated by conducting numerically simulated experiments rather than actual wind tunnel experiments. The simulations will be used to generate both free air and confined wind tunnel flow fields for each of the test articles over a range of test configurations. Specifically the pressure signature at the test section wall will be computed for the confined case to provide the simulated 'measured' data. These data will serve as the input for the WIAC method. The performance of the WIAC method then may be evaluated by comparing the corrected parameters with those for the free air simulation.
Document ID
19920006756
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lo, C. F.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Erickson, J. C.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Ulbrich, N.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-189785
NAS 1.26:189785
Report Number: NASA-CR-189785
Report Number: NAS 1.26:189785
Accession Number
92N15974
Funding Number(s)
CONTRACT_GRANT: NAG2-733
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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