Far-Term Noise Reduction Roadmap for the Midfuselage Nacelle Subsonic Transport

A noise reduction technology roadmap study is presented to determine the feasibility for the midfuselage nacelle (MFN) aircraft concept to achieve the noise goal set by NASA for the far-term timefr...

[1]  Russell H. Thomas,et al.  Progress of Aircraft System Noise Assessment with Uncertainty Quantification for the Environmentally Responsible Aviation Project , 2016 .

[2]  Y. P. Guo,et al.  PREDICTION OF FLAP SIDE EDGE NOISE , 1999 .

[3]  Michael Martinez,et al.  Determination of Combustor Noise from a Modern Regional Aircraft Turbofan Engine , 2006 .

[4]  Russell H. Thomas,et al.  Landing Gear Noise Prediction and Analysis for Tube-and-Wing and Hybrid-Wing-Body Aircraft , 2016 .

[5]  Thomas F. Brooks,et al.  Aeroacoustic Measurements of a Wing/Slat Model , 2002 .

[6]  Russell H. Thomas,et al.  Hybrid Wing–Body Aircraft Slat Noise , 2013 .

[7]  Eugene Chien,et al.  Folding Cavity Acoustic Liner for Combustion Noise Reduction , 2006 .

[8]  Russell H. Thomas,et al.  Quantification of Acoustic Scattering Prediction Uncertainty for Aircraft System Noise Assessment , 2016 .

[9]  Florence V. Hutcheson,et al.  A Comparison of the Noise Characteristics of a Conventional Slat and Krueger Flap , 2016 .

[10]  Kiyoshi Nagakura,et al.  Airframe Noise Studies on Wings with Deployed High Lift Devices , 1998 .

[11]  Jason C. June,et al.  Aircraft System Noise Prediction Uncertainty Quantification for a Hybrid Wing Body Subsonic Transport Concept , 2018, 2018 AIAA/CEAS Aeroacoustics Conference.

[12]  Leonard V. Lopes,et al.  Design of the Next Generation Aircraft Noise Prediction Program: ANOPP2 , 2011 .

[13]  Russell H. Thomas,et al.  Noise and Fuel Burn Reduction Potential of an Innovative Subsonic Transport Configuration , 2014 .

[14]  Jochen Wild,et al.  On the Noise Generation of Krueger Leading Edge Devices , 2015 .

[15]  Russell H. Thomas,et al.  Potential for Landing Gear Noise Reduction on Advanced Aircraft Configurations , 2016 .

[16]  Craig L. Nickol,et al.  Assessment of the Performance Potential of Advanced Subsonic Transport Concepts for NASA's Environmentally Responsible Aviation Project , 2016 .

[17]  Russell H. Thomas,et al.  On Noise Assessment for Blended Wing Body Aircraft , 2014 .

[18]  Michael Pott-Pollenske,et al.  Effect of Slat Gap/Overlap on Farfield Radiated Noise , 2003 .

[19]  Ricardo A. Burdisso,et al.  Wind Tunnel Aeroacoustic Measurements of a 26%-scale 777 Main Landing Gear , 2004 .

[20]  Eric Nesbitt,et al.  Quiet Technology Demonstrator 2 Intake Liner Design and Validation , 2006 .

[21]  David M. Elliott,et al.  Attenuation of FJ44 Turbofan Engine Noise With a Foam-Metal Liner Installed Over-the-Rotor , 2009 .

[22]  Russell H. Thomas,et al.  Aircraft Noise Reduction Technology Roadmap Toward Achieving The NASA 2035 Goal , 2017 .

[23]  Russell H. Thomas,et al.  Hybrid Wing Body Aircraft System Noise Assessment with Propulsion Airframe Aeroacoustic Experiments , 2010 .

[24]  Yueping Guo Aircraft Slat Noise Modeling and Prediction , 2010 .

[25]  Yueping Guo,et al.  Modeling and Prediction of Krueger Device Noise , 2016 .

[26]  Michael G. Jones,et al.  Evaluation of Novel Liner Concepts for Fan and Airframe Noise Reduction , 2016 .

[27]  W. Dobrzynski,et al.  Effect of Slat Gap on Farfield Radiated Noise and Correlation with Local Flow Characteristics , 2003 .