Computational Investigation of Vertical Stabilizer with Vortex Generators and Dorsal Fin

This paper describes methods to improve the performance of a vertical stabilizer in terms of yawing moment with corotating blade-type vortex generators and a dorsal fin over a wide range of sidesli...

[1]  Mitsuhiro Murayama,et al.  Wind Tunnel Interference Effects on Japan Aerospace Exploration Agency’s Standard Model , 2019, AIAA Scitech 2019 Forum.

[2]  Shunsuke Koike,et al.  Experimental Investigation of Vertical Stabilizer with Vortex Generators and Dorsal Fin , 2018, 2018 Applied Aerodynamics Conference.

[3]  David Hue,et al.  Experimental Investigations on the Common Research Model at ONERA-S1MA - Comparison with DPW Numerical Results , 2017 .

[4]  Fabrizio Nicolosi,et al.  Aerodynamic Design Guidelines of Aircraft Dorsal Fin , 2016 .

[5]  John C. Lin,et al.  An Overview of Active Flow Control Enhanced Vertical Tail Technology Development , 2016 .

[6]  Shunsuke Koike,et al.  Effect of Vortex Generators on Transonic Swept Wings , 2015 .

[7]  Yasushi Ito,et al.  Efficient and Accurate Evaluation of Aircraft in Different Configurations with Automatic Local Remeshing , 2013 .

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

[9]  Seigo Koga,et al.  80% Scaled NASA Common Research Model Wind Tunnel Test of JAXA at Relatively Low Reynolds Number , 2013 .

[10]  Michael Amitay,et al.  Performance Enhancement of a Vertical Stabilizer Using Synthetic Jet Actuators: Non-zero Sideslip , 2012 .

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

[12]  Ronald Slingerland,et al.  Aerodynamic Design of Transport Aircraft , 2009 .

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

[14]  John C. Vassberg,et al.  Development of a Common Research Model for Applied CFD Validation Studies , 2008 .

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

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

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

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

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

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

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

[22]  Steven B. Kern,et al.  Vortex flow control using fillets on a double-delta wing , 1993 .

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

[24]  N. G. Verhaagen,et al.  An experimental investigation of the vortex flow over delta and double-delta wings at low speed , 1983 .