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Semi-span model testing in the National Transonic FacilityThe objectives of the present research are: (1) to develop a computational approach to support semi-span model test techniques in the NTF; and (2) to integrate this approach with the conduct of an experimental test program. To meet these objectives, the following approach is taken. A state-of-the-art three-dimensional Navier-Stokes solver is employed to compute the flow over both a full-span configuration and a semi-span configuration mounted on the sidewall of the tunnel. The computations are validated by making direct comparisons to experimental data for both configurations. Then, the semi-span computational results are compared to the full-span results to document how the flow over the semi-span configuration differs from that over the full-span configuration. The results of this comparative study will be used to provide a conceptual framework within which a semi-spa model test technique may be implemented in the NTF.
Document ID
19960000910
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chokani, Ndaona
(North Carolina State Univ. Raleigh, NC, United States)
Milholen, William E., II
(North Carolina State Univ. Raleigh, NC, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-199272
NAS 1.26:199272
Report Number: NASA-CR-199272
Report Number: NAS 1.26:199272
Accession Number
96N10910
Funding Number(s)
CONTRACT_GRANT: NCC1-169
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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