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Minimum Vertical Tail DragTail size requirement calculations are presented for a vertical tail performing a coordinated turn reversal at corresponding load requirements with minimum tail drag.
Document ID
19760003941
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Larrabee, E. E. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Kansas Univ. Proc. of the NASA, Ind., Univ., Gen. Aviation Drag Reduction Workshop
Subject Category
Aerodynamics
Accession Number
76N11029
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19760003909Collected WorksProceedings of the NASA, Industry, University, General Aviation Drag Reduction Workshop
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