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A concept of the vortex lift of sharp-edge delta wings based on a leading-edge-suction analogyVortex lift calculation for sharp-edge delta wings based on leading edge suction analogy
Document ID
19670003842
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Polhamus, E. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3767
Report Number: NASA-TN-D-3767
Accession Number
67N13171
Funding Number(s)
CONTRACT_GRANT: 126-13-01-50-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VORTEX FLOW
DELTA WING
LIFT
SHARP LEADING EDGE

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