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Effect of Wing Tip Configuration on the Strength and Position of a Rolled-Up VortexEffect of wing tip configuration on strength and position of rolled-up vortex
Document ID
19700015145
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Padakannaya, R. (Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
August 5, 2013
Publication Date
March 1, 1970
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-66916
Report Number: NASA-CR-66916
Accession Number
70N24450
Funding Number(s)
CONTRACT_GRANT: NGR-39-009-111
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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