Journal of the Korean Society of Propulsion Engineers (한국추진공학회지)

The Korean Society of Propulsion Engineers (한국추진공학회)
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Aerodynamics Characteristics on a Canard-Controlled Projectile

카나드에 의하여 방향조종 되는 탄의 공력특성에 관한 실험적 연구

  • 박영하 (경상대학교 대학원 항공우주공학과) ;
  • 제상언 ((주)한화 종합연구소) ;
  • 조수용 (경상대학교 항공기부품기술연구센터)
  • Received : 2012.03.05
  • Accepted : 2012.12.20
  • Published : 2013.02.01
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Abstract

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 projectile. The angle of attack on the projectile was varied from $-5^{\circ}$ to $15^{\circ}$ and the roll angle of canard was changed from $0^{\circ}$ to $90^{\circ}$. The angle of attack on the canard was adjusted from $-20^{\circ}$ to $20^{\circ}$ and various inlet velocities were applied. Maximum Reynolds number based on the diameter of projectile was $5.5{\times}10^5$. The measured aerodynamic coefficients showed the same results for the various inlet velocities, and the highest effect on the canard was shown when the canard was set to the roll angle of $0^{\circ}$.

카나드에 의하여 방향조정 되는 탄에서, 여러 상황에 대응하는 공력계수의 값을 획득하기 위한 실험적인 연구를 아음속 풍동에서 수행하였다. 탄의 받음각은 $-5^{\circ}{\sim}15^{\circ}$ 까지 변경하였으며, 카나드의 롤각은 $0^{\circ}{\sim}90^{\circ}$ 까지 변경하였다. 방향 전환을 위한 카나드의 받음각은 $-20^{\circ}{\sim}20^{\circ}$ 까지 변경하였다. 여러 입구유속에서 시험을 수행하였으며, 모델의 직경을 기준으로 최대 레이놀즈수는 $5.5{\times}10^5$ 였다. 측정된 공력계수의 값들은 유속의 변화에 대하여 동일한 결과를 보여주었으며, 카나드 롤각이 $0^{\circ}$ 인 경우에 방향 전환을 위한 카나드의 효과가 가장 크게 나타났었다.

Keywords

References

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