NASA NTRS · 19930086550
Stieber Dynamometer Hub for Aircraft Propellers
Abstract
The knowledge gained from previous experiments and reports was utilized for the construction of a dynamometer hub for 200 mkg (134.4 ft.-lb.) and 1200 kg (2646 lb.) thrust suited for a Liberty "12" engine. A reversing device is also described.
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Stieber, W. 1924-11-01. Stieber Dynamometer Hub for Aircraft Propellers. https://ntrs.nasa.gov/citations/19930086550
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