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A simple approximation method for obtaining the spanwise lift distributionThe approximation method described makes possible lift-distribution computations in a few minutes. Comparison with an exact method shows satisfactory agreement. The method is of greater applicability than the exact method and includes also the important case of the wing with end plates.
Document ID
19930094469
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schrenk, O
Date Acquired
September 6, 2013
Publication Date
August 1, 1940
Report/Patent Number
NACA-TM-948
Accession Number
93R23389
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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