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Wall interference correction improvements for the ONERA main wind tunnelsThis paper describes improved methods of calculating wall interference corrections for the ONERA large windtunnels. The mathematical description of the model and its sting support have become more sophisticated. An increasing number of singularities is used until an agreement between theoretical and experimental signatures of the model and sting on the walls of the closed test section is obtained. The singularity decentering effects are calculated when the model reaches large angles of attack. The porosity factor cartography on the perforated walls deduced from the measured signatures now replaces the reference tests previously carried out in larger tunnels. The porosity factors obtained from the blockage terms (signatures at zero lift) and from the lift terms are in good agreement. In each case (model + sting + test section), wall corrections are now determined, before the tests, as a function of the fundamental parameters M, CS, CZ. During the windtunnel tests, the corrections are quickly computed from these functions.
Document ID
19830025637
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vaucheret, X.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1982
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.15:76971
NASA-TM-76971
Report Number: NAS 1.15:76971
Report Number: NASA-TM-76971
Accession Number
83N33908
Funding Number(s)
CONTRACT_GRANT: NASW-3541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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