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
Sonstige
Keine Angabe
Englisch
Static thrust of airplane propellers
NTRS | 1934
|Static thrust of airplane propellers
Engineering Index Backfile | 1932
|Static thrust of airplane propellers
TIBKAT | 1932
|Tests on propellers under static thrust conditions
TIBKAT | 1969
|Tests on Propellers under Static Thrust Conditions
NTIS | 1969
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