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Wind-tunnel investigation of a large 35 degree swept-wing jet transport model with an external-flow jet-augmented double-slotted flapWind tunnel tests of swept wing jet transport aircraft model with four pod mounted engines under wing and external flow, jet augmented double slotted flap
Document ID
19710023329
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Aoyagi, K. (NASA Ames Research Center Moffett Field, CA, United States)
Hall, L. P. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
A-3523
NASA-TN-D-6482
Report Number: A-3523
Report Number: NASA-TN-D-6482
Accession Number
71N32805
Funding Number(s)
CONTRACT_GRANT: 721-52-11-01-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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