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      KCI등재 SCIE SCOPUS

      Practical Applications of a Building Method to Construct Aerodynamic Database of Guided Missile Using Wind Tunnel Test Data

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      https://www.riss.kr/link?id=A105257534

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      다국어 초록 (Multilingual Abstract)

      A study of efficient aerodynamic database modeling method was conducted. A creation of database using periodicity and symmetry characteristic of missile aerodynamic coefficient was investigated to minimize the number of wind tunnel test cases. In addition, studies of how to generate the aerodynamic database when the periodicity changes due to installation of protuberance and how to conduct a zero calibration were carried out. Depending on missile configurations, the required number of test cases changes and there exist tests that can be omitted. A database of aerodynamic on deflection angle of control surface can be constituted using phase shift. A validity of modeling method was demonstrated by confirming that the result which the aerodynamic coefficient calculated by using the modeling method was in agreement with wind tunnel test results.
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      A study of efficient aerodynamic database modeling method was conducted. A creation of database using periodicity and symmetry characteristic of missile aerodynamic coefficient was investigated to minimize the number of wind tunnel test cases. In addi...

      A study of efficient aerodynamic database modeling method was conducted. A creation of database using periodicity and symmetry characteristic of missile aerodynamic coefficient was investigated to minimize the number of wind tunnel test cases. In addition, studies of how to generate the aerodynamic database when the periodicity changes due to installation of protuberance and how to conduct a zero calibration were carried out. Depending on missile configurations, the required number of test cases changes and there exist tests that can be omitted. A database of aerodynamic on deflection angle of control surface can be constituted using phase shift. A validity of modeling method was demonstrated by confirming that the result which the aerodynamic coefficient calculated by using the modeling method was in agreement with wind tunnel test results.

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      참고문헌 (Reference)

      1 Wernert P, "Wind tunnel tests and open-loop trajectory simulations for a 155mmcanards guided spin stabilized projectile" 18-21, 2008

      2 Oh YH, "Three dimensional interpolation method for missile aerodynamics, AIAA Paper 89-0481" 1989

      3 Kim CW, "The research on aerodynamic database for real time flight simulation of the tilt-rotor UAV" 2004

      4 Seo SE, "Store aerodynamic database enhancement by using missile DATCOM" 2010

      5 Guillaume S, "Modeling, identification and control of a guided projectile in a wind tunnel" Universite de Haute Alsace 2016

      6 진현, "KF-16의 DOE기반 정적 공력 데이터베이스 구축을 위한 실험적 연구" 한국항공우주학회 43 (43): 422-431, 2015

      7 Kokes J, "Generating an aerodynamic model for projectile flight simulation using unsteady, time accurate computational fluid dynamic results" Army Research Laboratory 2006

      8 MapleCG, "Aerodynamic symmetry of projectiles" 6 (6): 345-366, 1949

      9 Burchett BT, "Aerodynamic parameter identification for symmetric projectiles: comparing gradient based and evolutionary algorithms" 2011

      10 Burchett BT, "Aerodynamic parameter identification for symmetric projectiles: an improved gradient based method" 30 (30): 119-127, 2013

      1 Wernert P, "Wind tunnel tests and open-loop trajectory simulations for a 155mmcanards guided spin stabilized projectile" 18-21, 2008

      2 Oh YH, "Three dimensional interpolation method for missile aerodynamics, AIAA Paper 89-0481" 1989

      3 Kim CW, "The research on aerodynamic database for real time flight simulation of the tilt-rotor UAV" 2004

      4 Seo SE, "Store aerodynamic database enhancement by using missile DATCOM" 2010

      5 Guillaume S, "Modeling, identification and control of a guided projectile in a wind tunnel" Universite de Haute Alsace 2016

      6 진현, "KF-16의 DOE기반 정적 공력 데이터베이스 구축을 위한 실험적 연구" 한국항공우주학회 43 (43): 422-431, 2015

      7 Kokes J, "Generating an aerodynamic model for projectile flight simulation using unsteady, time accurate computational fluid dynamic results" Army Research Laboratory 2006

      8 MapleCG, "Aerodynamic symmetry of projectiles" 6 (6): 345-366, 1949

      9 Burchett BT, "Aerodynamic parameter identification for symmetric projectiles: comparing gradient based and evolutionary algorithms" 2011

      10 Burchett BT, "Aerodynamic parameter identification for symmetric projectiles: an improved gradient based method" 30 (30): 119-127, 2013

      11 Ahn SK, "Aerodynamic data base; wind tunnel or CFD" 2013

      12 Chapman GT, "A method for extracting aerodynamic coefficients from free-flight data" 8 (8): 753-758, 1970

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2023 평가예정 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
      2020-01-01 평가 등재학술지 유지 (해외등재 학술지 평가) KCI등재
      2013-10-01 평가 등재학술지 선정 (기타) KCI등재
      2011-01-01 평가 등재후보학술지 선정 (기타) KCI등재후보
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      학술지 인용정보

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      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.37 0.2 0.3
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.26 0.24 0.394 0.03
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