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Comparisons of one- and two- interface methods for tunnel wall interference calculationTunnel wall interference in two-dimensional subsonic flow can be analytically calculated on the basis of the one- or two-interface method. The application of numerical integration by means of matrix multiplication to both methods has been found to significantly reduce CPU time in on-line operation. An investigation of the sensitivity of these methods to random velocity-measurement disturbances shows the one-interface method to be less sensitive to measurement errors, and therefore to be preferable for practical applications.
Document ID
19900061906
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lo, C. F.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Ulbrich, N.
(Tennessee, University Tullahoma, United States)
Date Acquired
August 14, 2013
Publication Date
August 1, 1990
Publication Information
Publication: Journal of Aircraft
Volume: 27
ISSN: 0021-8669
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
ISSN: 0021-8669
Accession Number
90A48961
Funding Number(s)
CONTRACT_GRANT: NAG2-551
Distribution Limits
Public
Copyright
Other

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