| Stable, non-dissipative, and conservative flux-reconstruction schemes in split forms Y Abe, I Morinaka, T Haga, T Nonomura, H Shibata, K Miyaji Journal of Computational Physics 353, 193-227, 2018 | 45 | 2018 |
| Precooled turbojet engine flight experiment using balloon-based operation vehicle K Fujita, S Sawai, H Kobayashi, N Tsuboi, H Taguchi, T Kojima, K Okai, ... Acta Astronautica 59 (1-5), 263-270, 2006 | 41 | 2006 |
| An efficient correction procedure via reconstruction for simulation of viscous flow on moving and deforming domains C Liang, K Miyaji, B Zhang Journal of Computational Physics 256, 55-68, 2014 | 27 | 2014 |
| Computational study on effect of synthetic jet design parameters K Okada, A Oyama, K Fujii, K Miyaji International Journal of Aerospace Engineering 2010, 2010 | 22 | 2010 |
| High-order compact difference scheme applied to double-delta wing vortical flows T Arasawa, K Fujii, K Miyaji Journal of aircraft 41 (4), 953-957, 2004 | 17 | 2004 |
| Enhancement of the leading-edge separation vortices by trailing-edge lateral blowing K Miyaji, K Fujii, K Karashima AIAA journal 34 (9), 1943-1945, 1996 | 17 | 1996 |
| On Accuracy of Prediction of Flutter Boundaries on Unstructured Grids K Miyaji, H Tsukada, A Tsurumaki Transactions of the Japan Society for Aeronautical and Space Sciences 47 …, 2004 | 15 | 2004 |
| Computational Analysis of Vortex Structures Induced by a Synthetic Jet to Control Separated Flows. K Okada, T Nonomura, K Fujii, K Miyaji International Journal of Flow Control 4, 2012 | 13 | 2012 |
| Computational study of effects of nondimensional parameters on synthetic jets K Okada, A Oyama, K Fujii, K Miyaji Transactions of the Japan Society for Aeronautical and Space Sciences 55 (1 …, 2012 | 12 | 2012 |
| On the compressible flow simulations with shocks by a flux reconstruction approach K Miyaji 20th AIAA computational fluid dynamics conference, 3057, 2011 | 12 | 2011 |
| High-Lift devices for a Delta Wing installed around a Trailing-edge K Miyaji, T Arasawa Journal of aircraft 40 (5), 932-937, 2003 | 11 | 2003 |
| Numerical analysis of three-dimensional shock/shock interactions and the aerodynamic heating K Miyaji, K Fujii 37th Aerospace Sciences Meeting and Exhibit, 144, 1999 | 9 | 1999 |
| Transitional flow over a SD7003 wing using flux reconstruction scheme V Skarolek, K Miyaji 52nd Aerospace Sciences Meeting, 0250, 2014 | 8 | 2014 |
| Application of High-Order Compact Difference Scheme to Vortical Flow Computation over a Delta and Double-Delta Wings T Arasawa, K Fujii, K Miyaji 16th AIAA Computational Fluid Dynamics Conference, 3537, 2003 | 8 | 2003 |
| Program of High Mach Integrated Control Experiment,“HIMICO” using S-520 Sounding Rocket T Sato, H Taguchi, T Kojima, T Tsuchiya, M Tsue, S Nakaya, A Matsuo, ... TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES …, 2021 | 6 | 2021 |
| Prediction of aircraft dynamic stability derivatives using time-spectral computational fluid dynamics K Miyaji, Y Yoshida TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 62 (6 …, 2019 | 6 | 2019 |
| Aerodynamic design of balloon-based operation vehicle for precooled turbojet engine demonstration K Fujita, N Tsuboi, S Sawai, H Kobayashi, K Miyaji, T Uchiyama 15th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2008 | 6 | 2008 |
| WEB-CFD and beyond-CFD for non-CFD researchers K Fujii, K Miyaji 40th AIAA Aerospace Sciences Meeting & Exhibit, 753, 2002 | 6 | 2002 |
| Detached-Eddy Simulations of Synthetic Jets for High-Angles-of-Attack Airfoils Y Ishibashi, K Miyaji Journal of Aircraft 52 (1), 168-175, 2015 | 5 | 2015 |
| Vortical flow simulations by a high-order accurate unstructured hexahedral grid method K Miyaji Computers & Fluids 85, 78-84, 2013 | 5 | 2013 |
