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Full-scale Wind-tunnel Investigation of the Effects of Wing Modifications and Horizontal-tail Location on the Low-speed Static Longitudinal Characteristics of a 35 Degree Swept-wing Airplane
Document ID
19930087007
Document Type
Other
Authors
Maki, Ralph L
Date Acquired
August 16, 2013
Publication Date
April 3, 1952
Report/Patent Number
NACA-RM-A52B05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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NameType 19930087007.pdf STI