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Effects of Horizontal-tail Position, Area, and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degrees Triangular-wing Model Having Various Triangular-all-movable Horizontal Tails
Document ID
19930086998
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jaquet, Byron M
Date Acquired
August 16, 2013
Publication Date
December 14, 1951
Report/Patent Number
NACA-RM-L51I06
Report Number: NACA-RM-L51I06
Accession Number
93R16288
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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