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Development of an aerodyanmic theory capable of predicting surface loads on slender wings with vortex flowThe Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface method that shows promise in being able to accurately predict loads, subsonic and supersonic, on wings with leading-edge separation and reattachment.
Document ID
19770011056
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gloss, B. B. (NASA Langley Research Center Hampton, VA, United States)
Johnson, F. T. (Boeing Commercial Airplane Co. Seattle, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Proc. of the SCAR Conf., Part 1
Subject Category
Aerodynamics
Accession Number
77N18000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19770011052Collected WorksProceedings of the SCAR Conference, Part 1
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