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Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flapsA method of calculating the horizontal tail area for an airplane equipped with flaps is presented.. The general problem of tail design, the effects of flaps on the factors involved, and the manner in which the flaps change the requirements upon which the minimum horizontal tail area is based are discussed.
Document ID
19930081339
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Soule, Hartley A
Date Acquired
September 6, 2013
Publication Date
April 1, 1937
Report/Patent Number
NACA-TN-597
Report Number: NACA-TN-597
Accession Number
93R10629
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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