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Wall interference evaluation from pressure measurements on control surfacesConventional methods for the calculation of wall interference corrections are based on boundary conditions which require a knowledge of ventilated wall porosity parameters, and which are unsuitable for deformed walls. The method described uses a simple exponential decay of pressure distribution beyond the most upstream and downstream limits in order to evaluate Mach number and incidence corrections given by the method proposed by Papelier et al. (1978). It is found that, while the upstream contribution to incidence correction is significant, the upstream and downstream contributions to Mach number correction are negligible.
Document ID
19830031951
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Gopinath, R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
December 1, 1982
Publication Information
Publication: Journal of Aircraft
Volume: 19
Subject Category
Aerodynamics
Accession Number
83A13169
Distribution Limits
Public
Copyright
Other

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