Comparison of several inflow control devices for flight simulation of fan tone noise using a JT15D-1 engine
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1980-1025
Reference22 articles.
1. Evaluation of two inflow control devices for flight simulation of fan noise using a JT15D engine
2. Inlet turbulence and fan noise measured in an anechoic wind tunnel and statically with an inlet flow control device
3. Effectiveness of an inlet flow turbulence control device to simulate flight fan noise in an anechoic chamber
4. An investigation of possible causes for the reduction of fan noise in flight
5. An inflow turbulence reduction structure for scale model fan testing
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2. Design and Testing of Swept and Leaned Outlet Guide Vanes to Reduce Stator–Strut–Splitter Aerodynamic Flow Interactions;Journal of Turbomachinery;1999-07-01
3. Freestream turbulence effects on the development of a rotor wake;13th Fluid and PlasmaDynamics Conference;1980-07-14
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