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.
Stieber Dynamometer Hub for Aircraft Propellers
1924-11-01
Miscellaneous
No indication
English
Stieber Rollkupplung Kommanditgesellschaft
TIBKAT | 1961
|SAE Technical Papers | 1929
|Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929
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