Affiliation:
1. University of Cincinnati
2. GE Global Research
Publisher
American Institute of Aeronautics and Astronautics
Reference18 articles.
1. The distortion of a jet by tabs
2. Effect of tabs on the flow and noise field of an axisymmetric jet
3. 4Gliebe,P.R.,Brausch,J.F.,Majjigi,R.K.,Lee,R."JetNoiseSuppression,"AeroacousticsofFlightVehicles,ed. Hubbard, H.H., Vol.2, pgs.207-269, Acoustical Societyof America, 1995.
4. 5Saiyed,N.H.,Mikkelsen,K.L.,Bridges,J.E."AcousticsandThrustofSeparate-FlowExhaustNozzleswith MixingDevicesfor High-Bypass-Ratio Engines," AIAA-2000-0369.
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