Summary of JAXA Studies for the 2nd AIAA CFD High Lift Prediction Workshop Using Structured and Unstructured Mesh CFD
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Yasushi Ito | Mitsuhiro Murayama | Kazuomi Yamamoto | Tohru Hirai | Kentaro Tanaka | Yasushi Ito | M. Murayama | Kentaro Tanaka | T. Hirai | K. Yamamoto
[1] Kazuomi Yamamoto,et al. Turbulent Flow Solver Validation of FaSTAR and UPACS , 2014 .
[2] Yasushi Ito,et al. Summary of JAXA Studies for the Fifth AIAA CFD Drag Prediction Workshop Using UPACS and FaSTAR , 2013 .
[3] Kazuomi Yamamoto,et al. Comparison Study of Drag Prediction for the 4th CFD Drag Prediction Workshop using Structured and Unstructured Mesh Methods , 2010 .
[4] Kazuomi Yamamoto,et al. Comparison Study of Drag Prediction by Structured and Unstructured Mesh Method , 2008 .
[5] Mitsuhiro Murayama,et al. PIV Investigation of Nacelle Chine Effects on High-Lift System Performance , 2008 .
[6] Mitsuhiro Murayama,et al. Efficient Design Exploration of Nacelle Chine Installation in Wind Tunnel Testing , 2008 .
[7] Kazuomi Yamamoto,et al. Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel , 2008 .
[8] Kazuomi Yamamoto,et al. Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing , 2008 .
[9] S. Obayashi,et al. An Application of Local Correlation-Based Transition Model to JAXA High-Lift Configuration Model , 2007 .
[10] Mitsuhiro Murayama,et al. CFD Validation Study for a High-Lift Configuration of a Civil Aircraft Model , 2007 .
[11] Kazuhiro Nakahashi,et al. An Approach to Generate High Quality Unstructured Hybrid Meshes , 2006 .
[12] Z. Lei. Effect of RANS Turbulence Models on Computation of Vortical Flow over Wing-Body Configuration , 2005 .
[13] Kazuhiro Nakahashi,et al. Improvements in the reliability and quality of unstructured hybrid mesh generation , 2004 .
[14] R. Rudnik,et al. Overview About the European High Lift Research Programme EUROLIFT , 2004 .
[15] Kazuhiro Nakahashi,et al. Some challenges of realistic flow simulations by unstructured grid CFD , 2003 .
[16] Kazuhiro Nakahashi,et al. Surface triangulation for polygonal models based on CAD data , 2002 .
[17] C. P. van Dam,et al. The aerodynamic design of multi-element high-lift systems for transport airplanes , 2002 .
[18] Yasushi Ito,et al. Direct Surface Triangulation Using Stereolithography (STL) Data , 2000 .
[19] P. Spalart. Strategies for turbulence modelling and simulations , 2000 .
[20] K. Nakahashi,et al. Reordering of Hybrid Unstructured Grids for Lower-Upper Symmetric Gauss-Seidel Computations , 1998 .
[21] J. Dacles-Mariani,et al. Numerical/experimental study of a wingtip vortex in the near field , 1995 .
[22] S. Obayashi,et al. Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations , 1995 .
[23] V. Venkatakrishnan. Convergence to steady state solutions of the Euler equations on unstructured grids with limiters , 1995 .