All Stories

  1. Numerical Study of Flowfield Around a Multislotted High-Lift Wing

    Article • Journal of Aircraft, August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Yuichi Kuya, Prof. Keisuke Sawada

  2. Numerical Study of Transonic Shock Buffet Control over a Supercritical Airfoil

    Article • Journal of Aircraft, July 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Yuichi Kuya, Prof. Keisuke Sawada

  3. Computation of Turbulent Heat Flux with Roughness Induced Transition in High Enthalpy Shock Tunnel HIEST

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada, Hideyuki Tanno

  4. Improved Spectral Volume Method (SV+Method) for Hybrid Unstructured Mesh

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  5. High-Order Cellwise Relaxation Implicit Discontinuous Galerkin Scheme for Unsteady Flow Computations

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  6. Improvement in prediction capability of Transonic Buffet on NASA-CRM Using URANS

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  7. PIV

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Taro T I Imamura, Kisa Matsushima, Prof. Keisuke Sawada, Makoto Ueno, Takashi Aoyama

  8. An Attempt to Improve Prediction Capability of Transonic Buffet Using URANS

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  9. Wing Flutter Computation Using Modified Spectral Volume Method for Hybrid Unstructured Mesh

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  10. A Fourth Order Accurate Cellwise Relaxation Implicit Discontinuous Galerkin Scheme for Solving RANS Equations

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  11. Experimental Study on Heat Flux Augmentation in High-enthalpy Shock Tunnels

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada, Hideyuki Tanno

  12. Trajectory and Thermal Analysis for Disk-shaped Dust Particles through a Shock Layer

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  13. Numerical Analysis on Aerothermodynamic Characteristics of Blunt-nosed Cone in Free-piston Shock Tunnel HIEST

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada, Hideyuki Tanno

  14. Large Eddy Simulation of Pseudo-Shock Waves Using Wall Model

    Article • Open Journal of Fluid Dynamics, January 2014, Scientific Research Publishing, Inc,

    Prof. Keisuke Sawada

  15. Implicit Discontinuous Galerkin Method for RANS Simulation Utilizing Pointwise Relaxation Algorithm

    Article • Communications in Computational Physics, January 2009, Global Science Press

    Prof. Keisuke Sawada

  16. Diagnostics and Impulse Performance of Laser-Ablative Propulsion

    Article • January 2008, American Institute of Physics

    Prof. Keisuke Sawada

  17. Implicit LES of Compressible Turbulent Flow

    Article • January 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  18. Numerical Attempt for Capturing Wing Wake Flows

    Article • January 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  19. Comparative Study of Contact Surface Capturing Schemes

    Article • June 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  20. Effect of rotational nonequilibrium on shock standoff distances

    Article • January 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  21. Unified calculation of hypersonic flowfield for a reentry vehicle

    Article • January 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  22. Vibration-dissociation coupling effects on shock standoff distances

    Article • June 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  23. Calculation of intermediate hypersonic flow using multi-temperature model

    Article • January 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  24. Calculation of hypersonic flow with ablation for Pioneer-Venus probe

    Article • January 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  25. Calculation of nonequilibrium radiation from a blunt body shock layer

    Article • January 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  26. Convergence issues on fully-coupled radiative gas dynamic calculations

    Article • January 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  27. A flux difference multidimensional splitting scheme

    Article • November 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  28. Three-Stage Launch System with Scramjets

    Article • Journal of Spacecraft and Rockets, September 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  29. Calculation of shock shapes over simple geometry in intermediate hypersonic air flow

    Article • June 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  30. Calculation of surface heat transfer for a sphere with wall injection

    Article • January 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  31. Computation of hypersonic radiating flowfield over a blunt body

    Article • January 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  32. Behavior of two-temperature model in intermediate hypersonic regime

    Article • January 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  33. Numerical Study on the Underexpanded Coanda Jet

    Article • Journal of Aircraft, September 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  34. Nonequilibrium flow computation for the Space Shuttle nose using unstructured meshes

    Article • June 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  35. Assessment of Planck-Rosseland-Gray model for radiating shock layer

    Article • June 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  36. Validation of hypersonic equilibrium flow calculations using ballistic-range data

    Article • January 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  37. Conceptual study of an airbreathing reusable launch vehicle

    Article • January 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  38. Numerical study on the underexpanded Coanda jet

    Article • June 1996, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  39. A multi-dimensional extension of the preprocessing approach for cell-centered finite volume scheme

    Article • June 1991, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  40. Numerical investigation of supersonic inlet with realistic bleed andbypass systems

    Article • January 1991, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada

  41. Numerical Simulation of Compressible Flow Field about Complete ASKA Aircraft Configuration

    Article • December 1987, SAE International

    Prof. Keisuke Sawada

  42. A numerical investigation on wing/nacelle interferences of USB configuration

    Article • March 1987, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Keisuke Sawada