비정상 Euler 방정식을 이용한 동안정 미계수 예측

Prediction of Dynamic Stability Derivatives Using Unsteady Euler Equations

  • 박수형 (한국과학기술원 기계공학과 항공우주공학전공 대학원) ;
  • 김윤식 (한국과학기술원 기계공학과 항공우주공학전공 대학원) ;
  • 권장혁 (한국과학기술원 기계공학과 항공우주공학전공)
  • 발행 : 2001.05.01

초록

A dual-time stepping algorithm combined with a parallelized multigrid DADI method is presented to predict the dynamic damping coefficients. The Basic Finner model is chosen to validate the prediction capability of the present unsteady Euler method. The linearity of the pitch- and roll-damping coefficients is shown in the low angular rates and the interesting large drop and stiff increment in transonic region for roll-damping coefficients are explained in detail. Through the analysis for the pressure distributions at Mach number 1.0 to 1.2, the sudden drop results from the normal shock and the stiff increment of roll-damping reflects the transition of the normal shock to the oblique shock. The results also show that the Euler equations can give the damping coefficients with a comparable accuracy.

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