Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-propeller vtol model at static thrust
Propeller Slipstream Effects As Determined From Wing Pressure Distribution Of A Large-Scale Six-Propeller VTOL Model At Static Thrust
1962-12-01
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Englisch
Propeller Slipstream Development
British Library Conference Proceedings | 2007
|Static pressure in the slipstream of a propeller
AIAA | 1982
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