Proceedings of the KSME Conference (대한기계학회:학술대회논문집)

The Korean Society of Mechanical Engineers (대한기계학회)
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The Study of Aerodynamic Characteristics for the Ram-jet Projectile

렘제트탄의 공기역학적 특성 연구

  • 박순종 (충남대학교 기계공학과대학원) ;
  • 신필권 (충남대학교 기계공학과대학원) ;
  • 이택상 (충남대학교 기계공학과대학원) ;
  • 김경련 (충남대학교 기계공학과대학원) ;
  • 박종호 (충남대학교) ;
  • 김윤곤 (국방과학연구소)
  • Published : 2002.08.01
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Abstract

The SFU(Solid Fuel Ram-Jet) propulsion is attractive for projectiles because of the combination of high propulsive performance and low system complexity more than conventional projectiles. The Objective of this research was to characterize the inlet aerodynamic characteristics (centerbody & pilot type) in SFRJ. Diffuser static pressure & combustion chamber pressure was tested and the AoA was changed $0^{\circ}\;and\;4^{\circ}$ at Mach number of 3.0 for performance estimate. The performance study of inlet was carried out with the Schlieren system and Supersonic cold-flow system. A Computational fluid dynamic solution is applied internal flow of inlet and the solutions are compared with experimental results.

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