Japan Aerospace Exploration Agency’s and Kawasaki Heavy Industries’ Contribution to the Third High Lift Prediction Workshop

[1]  Makoto Ueno,et al.  Model Deformation Corrections of NASA Common Research Model Using Computational Fluid Dynamics , 2016 .

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

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

[4]  Mitsuhiro Murayama,et al.  Effect of a Nonlinear Constitutive Relation for Turbulence Modeling on Predicting Flow Separation at Wing-Body Juncture of Transonic Commercial Aircraft , 2012 .

[5]  Taku Nagata,et al.  Aeroacoustic Analysis of the Rudimentary Landing Gear Using Octree Unstructured Grid with Boundary-fitted Layer , 2012 .

[6]  Taku Nagata,et al.  Validation of new CFD tool using Non-orthogonal Octree with Boundary-fitted Layer Unstructured Grid , 2012 .

[7]  Alan M. Shih,et al.  Three‐dimensional automatic local remeshing for two or more hybrid meshes , 2011 .

[8]  Judith A. Hannon,et al.  Overview of the 1st AIAA CFD High Lift Prediction Workshop , 2011 .

[9]  C. L. Rumsey,et al.  Summary of the First AIAA CFD High Lift Prediction Workshop (invited) , 2011 .

[10]  Kidambi Sreenivas,et al.  A Parallel Universal Mesh Deformation Scheme , 2010 .

[11]  Kazuomi Yamamoto,et al.  Aerodynamic Influence of a Half-Span Model Installation for High-Lift Configuration Experiment , 2010 .

[12]  E. Shima,et al.  On New Simple Low-Dissipation Scheme of AUSM-Family for All Speeds , 2009 .

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

[14]  Kazuomi Yamamoto,et al.  Comparison Study of Drag Prediction by Structured and Unstructured Mesh Method , 2008 .

[15]  Kazuomi Yamamoto,et al.  Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel , 2008 .

[16]  Kazuomi Yamamoto,et al.  Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing , 2008 .

[17]  Christian B Allen,et al.  Parallel universal approach to mesh motion and application to rotors in forward flight , 2007 .

[18]  Takeshi Ito,et al.  High-Lift Device Testing in JAXA 6.5M X 5.5M Low-Speed Wind Tunnel , 2006 .

[19]  Mitsuhiro Murayama,et al.  Experiment and CFD of a High-lift Configuration Civil Transport Aircraft Model , 2006 .

[20]  Z. Lei Effect of RANS Turbulence Models on Computation of Vortical Flow over Wing-Body Configuration , 2005 .

[21]  Clarence O. E. Burg,et al.  Higher Order Variable Extrapolation For Unstructured Finite Volume RANS Flow Solvers , 2005 .

[22]  R. Rudnik,et al.  Overview About the European High Lift Research Programme EUROLIFT , 2004 .

[23]  Yves Le Sant,et al.  A model deformation method applied to PSP measurements , 2003, 20th International Congress on Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03..

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

[25]  P. Spalart Strategies for turbulence modelling and simulations , 2000 .

[26]  K. Nakahashi,et al.  Reordering of Hybrid Unstructured Grids for Lower-Upper Symmetric Gauss-Seidel Computations , 1998 .

[27]  J. Dacles-Mariani,et al.  Numerical/experimental study of a wingtip vortex in the near field , 1995 .

[28]  S. Obayashi,et al.  Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations , 1995 .

[29]  V. Venkatakrishnan Convergence to steady state solutions of the Euler equations on unstructured grids with limiters , 1995 .

[30]  P. Spalart A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .