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Application of the leading-edge-suction analogy of vortex lift to the drag due to lift of sharp-edge delta wingsSharp edge delta wing drag prediction by application of leading edge suction analogy of vortex lift
Document ID
19680022518
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
August 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4739
Report Number: NASA-TN-D-4739
Accession Number
68N31990
Funding Number(s)
CONTRACT_GRANT: 126-13-01-50-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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