‰ª–{@³l


‹qˆõ‹³ŽöE”ŽŽmiHŠwj

‰ª–{@³l

OKAMOTO Masato
ÅIXV“ú 2023/09/21

¡—ª—ð
2010”N
 
4ŒŽ
 
‹à‘òH‹Æ‘åŠw@HŠw•”@‹@ŠBŒn@q‹óƒVƒXƒeƒ€HŠw‰È@‹³Žö@

2018”N
 
4ŒŽ
 
‹à‘òH‹Æ‘åŠw@HŠw•”@q‹óƒVƒXƒeƒ€HŠw‰È@‹³Žö@

2023”N
 
4ŒŽ
 
‹à‘òH‹Æ‘åŠw@‹à‘òH‘匤‹†ƒZƒ“ƒ^[@q‹óƒVƒXƒeƒ€HŠwŒ¤‹†Š@‹qˆõ‹³Žö@



¡ê–啪–ì
ê–åFƒoƒCƒIƒƒJƒjƒNƒXA—ƒ“Á«A—¬‘Ì—ÍŠwAq‹óHŠw
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^@’mŠˆŽÉiPODj2022”N
ŽóÜF“ú–{q‹ó‰F’ˆŠw‰ï˜_•¶Üi2018”N4ŒŽjA“ú–{q‹ó‰F’ˆŠw‰ï˜_•¶Üi2023”N4ŒŽj
‚»‚Ì‘¼‚̐ê–åî•ñF‘æŽOŽí“d‹CŽå”C‹ZpŽÒA‘æ“ñŽí“d‹CHŽ–Žm

¡Œ¤‹†‹ÆÑ
‹ÆÑƒy[ƒW‚Ö