• 제목/요약/키워드: Aerodynamic Heating Rate

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Interaction of High-Speed Compressible Viscous Flow and Structure by Adaptive Finite Element Method

  • Limtrakarn, Wiroj;Dechaumphai, Pramote
    • Journal of Mechanical Science and Technology
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    • 제18권10호
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    • pp.1837-1848
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    • 2004
  • Interaction behaviors of high-speed compressible viscous flow and thermal-structural response of structure are presented. The compressible viscous laminar flow behavior based on the Navier-Stokes equations is predicted by using an adaptive cell-centered finite-element method. The energy equation and the quasi-static structural equations for aerodynamically heated structures are solved by applying the Galerkin finite-element method. The finite-element formulation and computational procedure are described. The performance of the combined method is evaluated by solving Mach 4 flow past a flat plate and comparing with the solution from the finite different method. To demonstrate their interaction, the high-speed flow, structural heat transfer, and deformation phenomena are studied by applying the present method to Mach 10 flow past a flat plate.

2축 김발 위에 장착된 비축탐색기를 위한 시선각속도 계산 (Line-of-Sight Rate for Off-axis Seeker on a 2-axis Gimbal)

  • 김정훈;박국권;유창경
    • 한국항공우주학회지
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    • 제47권3호
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    • pp.187-194
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    • 2019
  • 비축 적외선 탐색기는 공력 가열에 의한 열 차폐 효과를 완화시키기 위해 대공 고속 유도탄의 노즈콘 측면에 장착된다. 탐색기 출력은 표적을 지속적으로 추적하기 위한 유도탄의 롤 기동이 관여되었을 때 더 이상 시선각속도로 간주할 수 없다. 본 논문에서는 2축 김발 위에 장착된 비축탐색기를 위한 시선각속도 계산 방식을 제안한다. 첫째로, 실제 시선각속도 방정식은 해석적으로 도출되지만 조준각 오차 변화율을 측정할 수 없어 구현할 수 없다. 그에 따라 조준각 오차 변화율을 획득하기 위해 1차 지연 근사화를 제안한다. 제안한 시선각속도 계산 방식은 유도탄과 김발의 회전을 고려하여 커플링 효과를 보상할 수 있다. 제안한 방식의 성능을 비선형 6 자유도 시뮬레이션을 통해 검증하였다.

효율적인 냉각 방식 선정을 위한 탐색창 냉각 특성 해석 연구 (A Numerical Study on the Cooling Characteristics of Seeker Windows for Selecting Efficient Cooling Method)

  • 김만식;이동민
    • 한국군사과학기술학회지
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    • 제20권2호
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    • pp.246-254
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    • 2017
  • In this paper, cooling characteristics of seeker windows were examined using the Sinda-Fluint software. Various cooling methods were considered to satisfy the limit temperature of the cooled seeker window which would be exposed to excessive aerodynamic heating conditions by varying coolant type and mass flow rate of coolant. Due to the enhanced heat transfer between the coolant and the seeker window, internally cooled seeker window which uses liquid coolant showed lowered temperature distribution in the window compared to internally cooled seeker window which uses gas coolant. External film cooled seeker window also showed good cooling characteristics because it reduces the convective heat flux to the seeker window fundamentally. It was also confirmed that the temperature and the temperature gradient of seeker windows were significantly reduced for the cases which use external film cooling additionally to the gas and liquid cooled seeker window.