본문 바로가기
HOME> 논문 > 논문 검색상세

학위논문 상세정보

CFD-Fastran을 이용한 미사일 형상주위의 고속 유동장 연구 원문보기
Analysis of high speed flow field around a missile using CFD-fastran

  • 저자

    황성철

  • 학위수여기관

    慶尙大學校 産業大學院

  • 학위구분

    국내석사

  • 학과

    항공공학과

  • 지도교수

  • 발행년도

    2004

  • 총페이지

    vii, 47p.

  • 키워드

    CFD-Fastran 미사일형상주위 고속유동장 항공공학;

  • 언어

    kor

  • 원문 URL

    http://www.riss.kr/link?id=T10060305&outLink=K  

  • 초록

    In this study, aerodynamic characteristics of high-speed flow field around a missile are investigated using a commercial code CFD-FASTRAN. CFD-FASTRAN has been regarded as a powerful tool for very complicated steady and unsteady aerodynamic flow problems such as analysis of moving body, missile launch, and store separation. The validity of CFD-FASTRAN code was studied by comparing its results with wind tunnel test data and other calculation based on semi-empirical approach. It was observed that aerodynamic analysis using CFD-FASTRAN is easy to use and cost effective and the numerical results are in good agreement with other results in the case of the problems studied.


 활용도 분석

  • 상세보기

    amChart 영역
  • 원문보기

    amChart 영역