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A parametric wing design study for a modern laminar flow wingThe results of a parametric wing design study using a modern laminar flow airfoil designed to exhibit desirable stall characteristics while maintaining high cruise performance are presented. It was found that little is sacrificed in cruise performance when satisfying the stall margin requirements if a taper ratio of 0.65 or greater is used.
Document ID
19800006791
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Koegler, J. A., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-80154
Report Number: NASA-TM-80154
Accession Number
80N15050
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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