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Investigation of transonic flow over segmented slotted wind tunnel wall with mass transferThe flowfield on a segmented multi-slotted wind tunnel wall was studied at transonic speeds by measurements in and near the wall layer using five port cone probes. The slotted wall flowfield was observed to be three-dimensional in nature for a relatively significant distance above the slot. The boundary layer characteristics measured on the single slotted wall were found to be very sensitive to the applied suction through the slot. The perturbation in the velocity components generated due to the flow through the slot decay rapidly in the transverse direction. A vortex-like flow existed on the single slotted wall for natural ventilation but diminished with increased suction flow rate. For flow on a segmented multi-slotted wall, the normal velocity component changes were found to be maximum for measurement points located between the segmented slots atop the active chamber. The lateral influence due to applied suction and blowing, through a compartment, exceeded only slightly that in the downstream direction. Limited upstream influence was observed. Influence coefficients were determined from the data in the least-square sense for blowing and suction applied through one and two compartments. This was found to be an adequate determination of the influence coefficients for the range of mass flows considered.
Document ID
19910006668
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bhat, M. K.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Vakili, A. D.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Wu, J. M.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
UTSI-90
NAS 1.26:187760
NASA-CR-187760
Accession Number
91N15981
Funding Number(s)
CONTRACT_GRANT: NAG2-193
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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