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Smooth-Water Landing Stability and Rough-Water Landing and Take-Off Behavior of a 1/13-Scale Model of the Consolidated Vultee Skate 7 Seaplane, TED No. NACA DE 338A model of the Consolidated Vultee Aircraft Corporation Skate 7 seaplane was tested in Langley tank no. 2. Presented without discussion in this paper are landing stability in smooth water, maximum normal accelerations occurring during rough-water landings, and take-off behavior in waves.
Document ID
20050030039
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
McKann, Robert F. (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)
Arabian, Donald D. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 22, 2013
Publication Date
September 8, 1949
Subject Category
Aircraft Stability And Control
Report/Patent Number
NACA-RM-SL9H31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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