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Aeroelastic loads prediction for an arrow wing. Task 1: Evaluation of R. P. White's methodThe separated flow method is evaluated. This method was developed for moderately swept wings with multiple, constant strength vortex systems. The flow on the highly swept wing used in this evaluation is characterized by a single vortex system of continuously varying strength.
Document ID
19830013892
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Borland, C. J. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Manro, M. E. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1983
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
D6-51762-1
NAS 1.26:3640
NASA-CR-3640
Accession Number
83N22163
Funding Number(s)
CONTRACT_GRANT: NAS1-15678
PROJECT: RTOP 743-01-12-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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