Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Sang Eon Je"'
Autor:
Rho-Shin Myong, Byeong-Ju Yang, Dong-Gun Song, Je-Hyeon Jo, Sang-Eon Je, Yong-Seong Kang, Byeong-Kwan Kim
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 47:479-488
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 41:357-365
In this study, forces and moments were measured on a projectile which consisted of a missile configuration body(shell) and a head installed control fins. The shell and the head were separated each other and the shell was rotated by an electric motor.
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 17:42-51
An experimental study was conducted on a subsonic wind tunnel to obtain aerodynamic coefficients for various situations in order to control the direction of a p rojectile. The angle of attack on the projectile was varied from –5 o to 15 o and the r
An External Shape Optimization Study to Maximize the Range of a Guided Missile in Atmospheric Flight
Autor:
Sang Eon Je, Sang Bum Hu, Chan-Woo Park, Tae Hwan Cho, So Yeong Je, Rho-Shin Myong, Ui Chang Hwang, Young Rok Yang
Publikováno v:
Journal of the Korean Society for Aeronautical Space Science. 37:519-526
This paper describes a research result of a external shape optimization study to maximize the range of the guided missile with canards and tailfins in atmospheric flight. For this purpose, the external shape optimization program which can enhance the
Autor:
Tae-Hwan Cho, Jinseok Kim, Jin-Gyun Lee, Chan-Woo Park, Sang-Eon Je, Jae-Myong Lee, Do-Jun Kim
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 36:368-374
The basic Trainer Aircraft of The Korean Air force KT-1/KO-1, which was designed and developed by Korean Technology has been a primary candidate as a replacement for the aging basic trainer or armed version for surface support operation for the natio