Investigation proves that ratio of net static thrust on single engined airplane to propeller shaft thrust varied from 0.85 on high wing monoplane with several struts in slip stream to 0.95 on streamlined low wing monoplane.
Some full scale static propeller characteristics
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 5 , n 1
1937
4 pages
Article (Journal)
English
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