A Numerical Study of Aerodynamic Characteristics for a Rotating Parachute in Steady Descending Motion

등속도로 하강중인 Rotating Parachute의 공력특성에 관한 수치 해법 연구

  • 제상언 (경상대학교 대학원 항공공학과) ;
  • 정성기 (경상대학교 대학원 항공공학과) ;
  • 곽상혁 (한국항공우주산업(주)) ;
  • 명노신 (경상대학교 기계항공공학부) ;
  • 조태환 (경상대학교 기계항공공학부)
  • Published : 2005.04.01

Abstract

In this paper a method for analysing aerodynamic characteristics of a rotating parachute in steady descending motion is presented. Because of a complex geometric configuration of the parachute associated with side vents and discontinuous skirts, special procedure was adopted th handle the geometry in the analysis. A panel method was successfully applied to the present problem and yielded good results using above procedure. A CFD code using the full Navier-Stokes equations was also applied and provided good results. Parachute free drop and wind tunnel tests were performed to determine the fully developed canopy configuration and aerodynamic characteristics. The method can be used for optimizing the parachute size and side vent configurations in the design period.

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