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Tank Tests of the Effect of Rivet Heads, etc., on the Water Performance of a Seaplane Float, Special ReportA 1/3.5 full-size model of the Mark V float of the Bureau of Aeronautics, Navy Department, was tested in the NACA tank both with smooth painted bottom surfaces and with roundhead rivets, plate laps, and keel plates fitted to simulate the actual bottom of a metal float. The augmentation in water resistance due to the added roughness was found to be from 10-12% at the hum speed and from 12-14% at high speeds. The effect of the roughness of the afterbody was found to be negligible except at high trims. The model data were extrapolated to full size by the usual method which assumes the forces to vary according to Froude's law, and in the case of the smooth model by a method of separation that takes into account the effect of scale on the frictional resistance. It was concluded that the effect of rivet heads on the takeoff performance of a relatively high-powered float seaplane is of little consequence but that it may be of greater importance in the case of more moderately powered flying boats.
Document ID
20090014211
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Parkinson, J. B.
(Bureau of Aeronautics (Navy) Washington, DC, United States)
Robertson, J. B., Jr.
(Bureau of Aeronautics (Navy) Washington, DC, United States)
Date Acquired
September 7, 2013
Publication Date
June 4, 1936
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-SR-51
Report Number: NACA-SR-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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