Advanced turboprop wing installation effects measured by unsteady blade pressure and noise
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-2719
Reference18 articles.
1. Progress and trends in propeller/prop-fan noise technology
2. Whitlow, J.B. Jr. and Sievers, G.K. "Fuel Savings Potential of the NASA Advanced Turboprop Program,'' NASA TM-83736, 1984.
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