Airframe Noise Reduction of Flap Side-edge Using Vortex Generators

[1]  Yasushi Ito,et al.  Noise Reduction Design for Flap Side-edges toward FQUROH Second Flight Demonstration , 2017, 2018 AIAA/CEAS Aeroacoustics Conference.

[2]  Yasushi Ito,et al.  Acoustic Wind Tunnel Test with 18% Scale Half-span Model toward FQUROH Second Flight Demonstration , 2017, 2018 AIAA/CEAS Aeroacoustics Conference.

[3]  Kazuomi Yamamoto,et al.  Noise Reduction Design for Landing Gear toward FQUROH Flight Demonstration , 2017 .

[4]  Kazuomi Yamamoto,et al.  Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop , 2015 .

[5]  Shigemi Shindo,et al.  Noise Generation Characteristics of a High-lift Swept and Tapered Wing Model , 2013 .

[6]  Kazuomi Yamamoto,et al.  An Aerodynamic Noise Reduction Study for Airframe Noise from Flap Tips , 2013 .

[7]  Kazuomi Yamamoto,et al.  Numerical Investigation on Change of Airframe Noise by Flap Side-edge Shape , 2013 .

[8]  Alan M. Shih,et al.  Efficient Hybrid Surface/Volume Mesh Generation Using Suppressed Marching-Direction Method , 2013 .

[9]  Werner Dobrzynski,et al.  Almost 40 Years of Airframe Noise Research: What Did We Achieve? , 2010 .

[10]  Alan M. Shih,et al.  Efficient Computational Fluid Dynamics Evaluation of Small-Device Locations with Automatic Local Remeshing , 2009 .

[11]  Mitsuhiro Murayama,et al.  CFD Validation Study for a High-Lift Configuration of a Civil Aircraft Model , 2007 .

[12]  K. Nakahashi,et al.  Numerical Simulations on Separation of Scaled Supersonic Experimental Airplane from Rocket Booster at Supersonic Speed , 2002 .