Flight Test Results for Uniquely Tailored Propulsion- Airframe Aeroacoustic Chevrons: Community Noise
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[1] J. G. Shearin,et al. Shock structure and noise of supersonic jets in simulated flight to Mach 0.4 , 1988 .
[2] Russell H. Thomas,et al. Development of a Jet Noise Prediction Method for Installed Jet Configurations , 2003 .
[3] Kevin W. Kinzie,et al. Jet-Pylon Interaction of High Bypass Ratio Separate Flow Nozzle Configurations , 2004 .
[4] Russell H. Thomas,et al. Computational Analysis of a Chevron Nozzle Uniquely Tailored for Propulsion Airframe Aeroacoustics , 2006 .
[5] Steven Martens,et al. JET NOISE REDUCTION TECHNOLOGY DEVELOPMENT AT GE AIRCRAFT ENGINES , 2002 .
[6] M. Bull. Wall-pressure fluctuations associated with subsonic turbulent boundary layer flow , 1967, Journal of Fluid Mechanics.
[7] Vinod G. Mengle,et al. Reducing Propulsion Airframe Aeroacoustic Interactions With Uniquely Tailored Chevrons: 3. Jet-Flap Interaction , 2006 .
[8] Eric Nesbitt,et al. A NOVEL ONSITE NARROWBAND TOOL FOR FLIGHT TEST ACOUSTIC DATA PROCESSING , 2002 .
[9] Stefan Uellenberg,et al. The Quiet Technology Demonstrator Program: Flight Validation of Airplane Noise-Reduction Concepts , 2006 .
[10] Eric Nesbitt,et al. Effect of Uniform Chevrons on Cruise Shockcell Noise , 2006 .
[11] Vinod G. Mengle,et al. Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 1. Isolated Nozzles , 2018 .
[12] Dean Long. Effect of Nozzle Geometry on Turbofan Shock Cell Noise at Cruise , 2005 .
[13] Thonse R. S Bhat. Experimental study of acoustic characteristics of jets from dual flow nozzles , 2001 .
[14] Eric Nesbitt,et al. Flight Test Results for Uniquely Tailored Propulsion- Airframe Aeroacoustic Chevrons: Shockcell Noise , 2006 .
[15] Russell H. Thomas,et al. Computational and Experimental Flow Field Analyses of Separate Flow Chevron Nozzles and Pylon Interaction , 2003 .
[16] Krishna Viswanathan,et al. Parametric study of noise from dual-stream nozzles , 2003, Journal of Fluid Mechanics.
[17] Ronen Elkoby. Full-Scale Propulsion Airframe Aeroacoustics Investigation , 2005 .
[18] Christopher K. W. Tam,et al. Shock associated noise of supersonic jets from convergent-divergent nozzles , 1982 .
[19] W. N. Dalton,et al. AST Critical Propulsion and Noise Reduction Technologies for Future Commercial Subsonic Engines: Separate-Flow Exhaust System Noise Reduction Concept Evaluation , 2000 .
[20] Eric Nesbitt,et al. CORRELATING MODEL-SCALE & FULL-SCALE TEST RESULTS OF DUAL FLOW NOZZLE JETS , 2002 .
[21] Ulrich Ganz,et al. Acoustic and Flow-Field Characteristics of Shock-cell Noise from Dual Flow Nozzles , 2005 .