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Lift distribution in a rectangular jetComputer programs predict effect of slipstream-wing flow interaction on aerodynamic characteristics of deflected slipstream and tilt aircraft. One program calculates lift distribution, lift, and drag of wing in wide slipstream. Results permit development of simplified lifting surface theory for circular jet.
Document ID
19710000030
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Jameson, A. (GRUMMAN AEROSPACE CORP.)
Date Acquired
August 6, 2013
Publication Date
February 1, 1971
Subject Category
Mathematics And Information Sciences
Report/Patent Number
ARC-10424
Report Number: ARC-10424
Accession Number
71B10030
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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