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Trimmed noncoplanar planforms with minimum vortex dragVortex-lattice subsonic method determines mean camber surface for trimmed noncoplanar planforms with minimum vortex drag. Multiple surfaces can be designed together to yield trimmed configuration with minimum induced drag at some specified lift coefficient. Program is applicable to isolated wings, wing-canard configuration, tandem wing, and wing-winglet configuration.
Document ID
19760000566
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Lamar, J. E.
Date Acquired
August 8, 2013
Publication Date
March 1, 1977
Publication Information
Publication: NASA Tech Briefs
Volume: 1
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12121
Accession Number
76B10566
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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