Environmentally Responsible Aviation - Real Solutions for Environmental Challenges Facing Aviation
暂无分享,去创建一个
Russell H. Thomas | Casey L. Burley | Craig L. Nickol | F Collier | C M Lee | Russell H. Thomas | C. Burley | F. Collier | C. Lee
[1] Dimitri Papamoschou,et al. Numerical Study of Noise Shielding by Airframe Structures , 2008 .
[2] Kevin W. Kinzie,et al. Jet-Pylon Interaction of High Bypass Ratio Separate Flow Nozzle Configurations , 2004 .
[3] Russell H. Thomas,et al. Computational Analysis of a Chevron Nozzle Uniquely Tailored for Propulsion Airframe Aeroacoustics , 2006 .
[4] Russell H. Thomas,et al. Flight Test Results for Uniquely Tailored Propulsion- Airframe Aeroacoustic Chevrons: Community Noise , 2006 .
[5] D Joslin Ronald,et al. Overview of Laminar Flow Control , 1998 .
[6] Tom Hynes,et al. Performance of a Boundary Layer Ingesting (BLI) propulsion system , 2007 .
[7] William L. Sellers,et al. Riblet drag reduction at flight conditions , 1988 .
[8] Dawn C. Jegley,et al. Airframe Development for the Hybrid Wing Body Aircraft , 2009 .
[9] Markus Lummer,et al. Maggi-Rubinowicz Diffraction Correction for Ray-Tracing Calculations of Engine Noise Shielding , 2008 .
[10] Russell H. Thomas,et al. Computational and Experimental Flow Field Analyses of Separate Flow Chevron Nozzles and Pylon Interaction , 2003 .
[11] Ana F. Tinetti,et al. Application of Fast Multipole Methods to the NASA Fast Scattering Code , 2008 .
[12] Carl H. Gerhold,et al. Inlet Noise Reduction by Shielding for the Blended-Wing-Body Airplane , 1999 .
[13] Mark Drela,et al. Airframe Design for "Silent Aircraft" , 2007 .
[14] Russell H. Thomas,et al. Hybrid Wing Body Aircraft System Noise Assessment with Propulsion Airframe Aeroacoustic Experiments , 2010 .
[15] Boeing Phantom,et al. SUBSYSTEM DESIGN AND INTEGRATION FOR THE MORE ELECTRIC AIRCRAFT , 2007 .
[16] Craig A. Reimann,et al. Noise Scattering by the Blended Wing Body Airplane: Measurements and Prediction , 2006 .
[17] Robert Liebeck,et al. BLENDED-WING-BODY SUBSONIC COMMERCIAL TRANSPORT , 1998 .
[18] Vinod G. Mengle,et al. Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 1. Isolated Nozzles , 2018 .
[19] Keith Hunten,et al. A Systems MDO Approach for an Unmanned Aerial Vehicle , 2007 .
[20] Fereidoun Farassat,et al. Effects of Bifurcations on Aft-Fan Engine Nacelle Noise , 2004 .
[21] Cesare A. Hall,et al. Challenges in the silent aircraft engine design , 2007 .
[22] Robert P. Dougherty. A parabolic approximation for flow effects on sound propagation in nonuniform, softwall, ducts , 1999 .
[23] Joshua E. Freeh,et al. Solid Oxide Fuel Cell/Gas Turbine Hybrid Cycle Technology for Auxiliary Aerospace Power , 2005 .
[24] W. E. Zorumski. Aircraft noise prediction program theoretical manual, part 1 , 1982 .
[25] Y. Miyazawa,et al. Gust load alleviation of a transport-type wing - Test and analysis , 1989 .
[26] Ronald T. Kawai. Acoustic Prediction Methodology and Test Validation for an Efficient Low-Noise Hybrid Wing Body Subsonic Transport , 2011 .
[27] Karl A. Geiselhart,et al. Integration of Propulsion-Airframe-Aeroacoustic Technologies and Design Concepts for a Quiet Blended-Wing-Body Transport , 2004 .
[28] Zyun-iti Maekawa,et al. Noise reduction by screens , 1968 .
[29] Michael J. Siclari,et al. Optimization of segmented flaps for in-flight transonic performance enhancement , 1997 .
[30] Massimo Santarelli,et al. Analysis of Solid Oxide Fuel Cell Systems for More-Electric Aircraft , 2009 .
[31] Craig L. Nickol,et al. Hybrid Wing Body Configuration System Studies , 2009 .
[32] Steven Martens,et al. JET NOISE REDUCTION TECHNOLOGY DEVELOPMENT AT GE AIRCRAFT ENGINES , 2002 .
[33] Geoffrey A. Hill,et al. Challenges and Opportunities for Noise Reduction Through Advanced Aircraft Propulsion Airframe Integration and Configurations , 2005 .
[34] Russell H. Thomas,et al. Development of a Jet Noise Prediction Method for Installed Jet Configurations , 2003 .
[35] Thonse R. S Bhat. Experimental study of acoustic characteristics of jets from dual flow nozzles , 2001 .
[36] Edmane Envia,et al. An Analytical Assessment of NASA's N+1 Subsonic Fixed Wing Project Noise Goal , 2009 .
[37] Russell H. Thomas,et al. Propulsion Airframe Aeroacoustic Integration Effects for a Hybrid Wing Body Aircraft Configuration , 2010 .
[38] Mark Page,et al. Blended Wing Body analysis and design , 1997 .