Aeroacoustic Effects of Reduced Aft Tip Speed at Constant Thrust for A Model Counterrotation Turboprop at Takeoff Conditions

Aeroacoustic Effects of Reduced Aft Tip Speed at Constant Thrust for A Model Counterrotation Turboprop at Takeoff Conditions

Microform - 1990
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Publisher: [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
Characteristics: 1 v
Additional Contributors: Hughes, Christopher E.
United States

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