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Accumulated span loadings of an arrow wing having vortex flowThe vortex flow over an arrow wing is theoretically investigated using the free-vortex-sheet method. The sectional lift coefficient and accumulated span loadings, which are important in determining the root bending moment, are calculated. The longitudinal stability variation is also estimated.
Document ID
19900025970
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Reddy, C. Subba (Union College Schenectady, NY, United States)
Date Acquired
August 14, 2013
Publication Date
November 1, 1989
Publication Information
Publication: Journal of Aircraft
Volume: 26
ISSN: 0021-8669
Subject Category
Aerodynamics
Accession Number
90A13025
Funding Number(s)
CONTRACT_GRANT: NAS1-14193
Distribution Limits
Public
Copyright
Other

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