4E3 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS TECHNICAL EXPERIMENTAL

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Date: 2010-01-06 16:42:34 Airfoil Pitching moment Lift coefficient Disk loading Turbine Helicopter Stall Blade pitch Helicopter rotor Aerodynamics Aerospace engineering Fluid dynamics		4E3 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS TECHNICAL EXPERIMENTAL Add to Reading List Source URL: crgis.ndc.nasa.gov Download Document from Source Website File Size: 1,30 MB Share Document on Facebook

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