• 제목/요약/키워드: Damaged Airfoil

검색결과 2건 처리시간 0.014초

화포에 의해 손상된 날개의 공력특성에 관한 연구 (A Study on the Aerodynamic Characteristic of Gunfire Damaged Airfoil)

  • 이기영;정형석;김시태
    • 한국군사과학기술학회지
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    • 제11권2호
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    • pp.144-151
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    • 2008
  • An experimental study has been conducted to investigate the effects of circular damage hole on the characteristics of airfoil performance. The damage on a wing created from a hit by anti-air artillery was modeled as a circular hole. Force balance measurements and static pressure measurements on the wing surface were carried out for the cases of having damage holes of 10% chord size at quarter chord and/or half chord positions. All experiments were conducted at Reynolds number of $2.85\times10^5$ based on the chord length. The surface pressure data show big pressure alterations near the circular damage holes. This abnormal surface pressure distribution produces shear stress that could lead to the acceleration of the structural degradation of the wing around the circular damage hole. However, in spite of the existence of circular damage holes, the measured force data indicated the only a slight decrease in lift accompanied by increase in drag compared to the results of undamaged one. The influence of damage hole on the aerodynamic performance was increased as the location of damage moved to the leading edge. The effect on the control force was insignificant when the damaged size was not large.

낮은 속도비에서의 직렬 이중 제트-교차흐름의 유동 구조 (The Flow Field Structures of In-lined Double Jet-in-Cross Flow at Low Velocity Ratio)

  • 이기영
    • 한국군사과학기술학회지
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    • 제18권4호
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    • pp.415-422
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    • 2015
  • The flow field structures of dual jet-in-cross-flow were examined experimentally for in-lined perforated damage holes configuration using particle image velocimetry. Ensemble averaged in-plane velocity and vorticity data in the jet were determined to study the mean jet structure. Jets are formed by pressure differences between upper and lower airfoil surface. The flow structure of vicinity of the thru holes consist of a vortical structure that wrap around the jets like a horseshoe and develop further downstream through a pair of stream-wise vortices. The shape, size and location of the horseshoe vortex were found to be dependent on the angle of attack. In spite of the existence of battle damage holes, the effect on the control force was insignificant when the damage size was not large enough.