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Data from Tests of a 1/5-Scale Model of a Proposed High-Speed Submarine in the Langley Full-Scale TunnelTests of a 1/5 scale model of a proposed 153-foot high-speed submarine have been conducted in the Langley full-scale tunnel at the request of the Bureau of Ships, Department of the Navy. The test program included: (1) force tests to determine the drag, control effectiveness, and static stability characteristics for a number of model configurations, both in pitch and in yaw, (2) pressure measurements to determine the boundary-layer conditions and flow characteristics in the region of the propeller, and (3) an investigation of the effects of propeller operation on the model aerodynamic characteristics. In response to oral requests from the Bureau of Ships representatives t hat the basic data obtained in these tests be made available to them as rapidly as possible, this data report has been prepared to present some of the more pertinent results. All test results given in the present paper are for the propeller-removed condition and were obtained at a Reynolds number of approximately 22,300,000 based on model length.
Document ID
20090026505
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Cocke, Bennie W.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Lipson, Stanley
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Scallion, William I.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 24, 2013
Publication Date
May 9, 1950
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NACA-RM-SL50E09a
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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