Static thrust and power measurements were made of six full-scale propellers. The propellers were mounted in front of a liquid-cooled-engine nacelle and were tested at 15 different blade angles in the range from -7 1/2 degrees to 35 degrees at 0.75r. The test rig was located outdoors and the tests were made under conditions of approximately zero wind velocity.
Static Thrust and Power Characteristics of Six Full-Scale Propellers
1940-01-01
Miscellaneous
No indication
English
Static thrust and power characteristics of six full-scale propellers
Engineering Index Backfile | 1940
|Static thrust of airplane propellers
NTRS | 1934
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Engineering Index Backfile | 1932
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