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ÅIXV“ú 2024/10/16 ¡—ª—ð 2010”N 4ŒŽ ‹à‘òH‹Æ‘åŠw@HŠw•”@‹@ŠBŒn@q‹óƒVƒXƒeƒ€HŠw‰È@‹³Žö@ 2018”N 4ŒŽ ‹à‘òH‹Æ‘åŠw@HŠw•”@q‹óƒVƒXƒeƒ€HŠw‰È@‹³Žö@ 2023”N 4ŒŽ ‹à‘òH‹Æ‘åŠw@‹à‘òH‘匤‹†ƒZƒ“ƒ^[@q‹óƒVƒXƒeƒ€HŠwŒ¤‹†Š@‹qˆõ‹³Žö@ ¡ê–啪–ì ê–åFƒoƒCƒIƒƒJƒjƒNƒXA—ƒ“Á«A—¬‘Ì—ÍŠwAq‹óHŠw Žå‚Ș_•¶E’˜‘F EOkamoto, M. and Ebina, K., gEffectiveness of Large-Camber Circular Arc Airfoil at Very Low Reynolds Numbers,h Trans. Jpn. Soc. Aeronaut. Space Sci., 59, 5, 2016, pp.295-304 EOkamoto, M., Fukatsu, S. and Sasaki, D., gMeasurement of Unsteady Aerodynamic Characteristics of a Heaving Wing in a Low Reynolds Number Flow,h Trans. Jpn. Soc. Aeronaut. Space Sci., 64, 3, 2021, pp.147-155 ’˜‘F©’ŽƒTƒCƒY—ƒ‚Ì‹ó—̓f[ƒ^@’mŠˆŽÉiPODj2022”N ŽóÜF“ú–{q‹ó‰F’ˆŠw‰ï˜_•¶Üi2018”N4ŒŽjA“ú–{q‹ó‰F’ˆŠw‰ï˜_•¶Üi2023”N4ŒŽj ‚»‚Ì‘¼‚Ìê–åî•ñF‘æŽOŽí“d‹CŽå”C‹ZpŽÒA‘æ“ñŽí“d‹CHŽ–Žm ¡Œ¤‹†‹ÆÑ ‹Æуy[ƒW‚Ö |