Propellers were mounted in front of liquid cooled engine nacelle and were tested at 15 different blade angles in range from -7 1/2° to 35° at 0.75R; test rig was located outdoors and tests were made under conditions of approximately zero wind velocity; airfoil characteristics computed from statictest data, were considerably different from airfoil characteristics computed from wind tunnel test data.
Static thrust and power characteristics of six full-scale propellers
Nat Advisory Committee Aeronautics -- Report
1940
16 pages
Report
Englisch
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Static thrust of airplane propellers
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