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The Dynamometer Hub for the Testing Propellers and Engines During FlightThe need for a device to measure flight resistance, engine and propeller power, and efficiency during flight grew in proportion to the demand for increased flying capacity in military types of aircraft. Here, a dynamometer hub was inserted between the engine and the propeller. Taken as a whole, the tests that were conducted show that though the dynamometer is a sensitive instrument liable to numerous derangements, it is undeniably useful even in its present form, when handled with care and skill. Facilitating, as it does, the possibility of maintaining the fixed position of the engine, the blocking out of the weight effect when the plane is in the sloping position, and the possibility of taking direct measurements of force at the point of transmission, the dynamometer appears to be by far the best solution of the problem of a flying test bench, utilized as a hydraulic balance with the smallest possible measuring stroke and the least tendency to oscillation.
Document ID
19930080839
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Enoch, O
Date Acquired
September 6, 2013
Publication Date
July 1, 1921
Report/Patent Number
NACA-TN-59
Report Number: NACA-TN-59
Accession Number
93R10129
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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