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Take-off Stability Characteristics of a 1/13-scale Model of the Consolidated Vultee Skate 7 Seaplane (TED No. NACA DE 338)The take-off stability characteristics of a Consolidated Vultee Aircraft Corporation Skate 7 seaplane were determined in the Langley tank no. 2. Trim limits of stability, trim tracks, and elevator limits of stability are presented.
Document ID
20090026464
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
McKann, Robert
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Coffee, Claude W.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Abrabian, Donald D.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 24, 2013
Publication Date
April 27, 1949
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-RM-SL9D28a
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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