Thermal behavior of the duct applied Functionally Graded Material

경사기능재료를 적용한 덕트의 열적거동해석

  • 윤동영 (한국항공대학교 대학원) ;
  • 박정선 (한국항공대학교 항공우주 및 기계공학부) ;
  • 임종빈 (한국항공대학교 항공우주 및 기계공학부)
  • Published : 2004.11.03

Abstract

In unmanned aerial vehicles (UAV), the high temperature results from friction among the air, combustion of fuel in engine and combustion gas of a nozzle. The high temperature may cause serious damages in UAV structure. The Functionally Graded Material (FGM) is chosen as a material of thc engine duct structure. Thermal stress analysis of FGM is performed in this paper. FGM is composed of two constituent materials that are mixed up according to the specific volume fraction distribution in order to withstand high temperature. Therefore, hoop stress, axial stress and shear stress of duct with 2 layers, 4 layers and 8 layers FGM are compared and analyzed respectively. In addition, the creep behavior of FGM used in duct structure of an engine is analyzed for better understanding of FGM characteristics.

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