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The Scale Effect in Towing Tests with Airplane-float SystemsThe present report includes a description of the making of three-component measurements on a full-size float mounted on an actual airplane and the comparison of the results with those from two models of the same form but of different size which had been tested in the towing tank. The purpose of the comparison is to determine the effect of the Reynolds Number on the results of model tank tests. Following a brief discussion of previous tests intended to elucidate the problem of scale effect on float systems and a description of the testing equipment, the choice of the reference quantities to be used in the comparison is discussed. The selection of load, speed, and trim as a basis of comparison seems best suited to the practical operation of making this comparison. The quantities affected by scale are then: resistance, trimming moment, and their derivatives; planing number (resistance/weight on water); and position of center of pressure.
Document ID
19930094590
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schmidt, Rudolph
Date Acquired
September 6, 2013
Publication Date
May 1, 1937
Report/Patent Number
NACA-TM-826
Report Number: NACA-TM-826
Accession Number
93R23510
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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