最終報告書（資料編） - 東北大学流体科学研究所

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Numerical and Experimental Studies of Flap-tip Flowfield Aimed at Reducing the Noise of a Civil Transport Aircraft Suppression of Cavity Noise by Active Control Device( Wing Rock Measurement-Integrated Simulation of Air Turbulence toward Improvement in Aviation Safety K. Nakahashi, Y. Ito, F. Togashi, “Some challenges of realistic flow simulations by unstructured grid CFD”, Int. J. Numer. Mech. Fluids, Vol.43, pp.769-783, 2003. Murayama, M., Nakahashi, K., Matsushima, K., “A Robust Method for Unstructured Volume/Surface Mesh Movement,” Transaction of the Japan Society for Aeronautical and Space Sciences, Vol. 46, No. 152, August 2003, pp. 104-112. LaeSung KIM, Kazuhiro NAKAHASHI, “Navier-Stokes Computations of Multi-Element Airfoils”, Computational Fluid Dynamics JOURNAL, Vol.12 No.1, April 2003, pp.107-114. “Aerodynamic -24-
Optimization of Supersonic Transport”51 597 2003 10 pp.577-581. Takeshi Fujita, Kisa Matsushima, Kazuhiro Nakahashi, “Aerodynamic Wing Design of NEXST-2 Using Unstructured-Mesh and Supersonic Inverse Problem”, Journal of Aircraft, Vol. 40, No. 6, November 2003. Kisa Matsushima, Wataru Yamazaki , Kazuhiro Nakahashi, “TRANSONIC DESIGN OF SST - To Employ Japanese SST as a Candidate for Near Sonic Transport,” Fluid Mechanics and Application, Vol.73, H. Sobieczky (ed.), Kluwer Academic Publishers, November, 2003, pp.317-324. K. Matsushima, T. Iwamiya, K. Nakahashi, “Wing design for supersonic transport using integral equation method”, Enginnering Analysis with Bondary Elements 28, pp.247-255 (2004). Ito, Y., Nakahashi, K., “Improvements in the Reliability and Quality of Unstructured Hybrid Mesh Generation,” Int. J. for Numerical Methods in Fluids, 45, pp.79-108, 2004. T. Fujita, K. Matsushima, K. Nakahashi, “Aerodynamic Wing Desing of NEXST-2 Using Unstructured-Mesh and Supersonic Inverse Problem”, J. of Aircraft, 41, pp.1146-1152, 2004. M. Murayama, K. Nakahashi, K. Yamamoto, T. Iwamiya, “Simulation of Aircraft with Changing Control Surface Deflection at Near-Sonic Speed”, CFD J. 13(2), pp.295-303, 2004. Wataru YAMAZAKI, Kisa MATSUSHIMA, Kazuhiro NAKAHASHI,“Drag Prediction and Decomposition Based on CFD Computations”, JSME International JournalSeries B, 48 , pp.235-240,2005. Mitsuhiro Murayama, Fumiya Togashi, Kazuhiro Nakahashi, Kisa Matsushima and Takuma Kato,“Simulation of Aircraft response to Control Surface Deflection Using Unstructured Dynamic Grids”, Journal of Aircraft, 42, pp.340-346, 2005. Wataru Yamazaki, Kisa Matsushima, Kazuhiro Nakahashi,“Drag Reduction of a Near-Sonic Airplane Using Computational Fluid Dynamics”, AIAA Journal, 43, pp.1870-1877, 2005. CFD (Journal of Japan Society of Fluid Dynamics), 24, pp.525-533,2005. H. J. Kim, S. Koc and K. Nakahashi, “Surface Modification Method for Aerodynamic Design Optimization,” AIAA J., Vol. 43, No. 4, pp. 727-740, 2005. H. J. Kim and K. Nakahashi, “Unstructured Adjoint Method for Navier-Stokes Equations,” JSME International J. Series B, Vol. 48, No.2, pp. 202-207, 2005. -25-
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最終報告書（資料編） - 東北大学流体科学研究所