한국전산유체공학회:학술대회논문집

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
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AN ANALYSIS OF THE AERODYNAMIC CHARACTERISTICS OF A T-50 CONFIGURATION USING A PANEL CODE AND ITS VALIDATION

패널코드를 이용한 T-50 형상의 공력특성 예측 및 검증

  • 박선욱 (항공우주산업(주)) ;
  • 김도준 (경상대학교 대학원 항공공학과) ;
  • 제상언 (경상대학교 대학원 항공공학과) ;
  • 명노신 (경상대학교 기계항공공학부 및 항공기부품기술연구소) ;
  • 조태환 (경상대학교 기계항공공학부 및 항공기부품기술연구소)
  • Published : 2006.10.13
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Abstract

The aerodynamic characteristics of a T-50 aircraft configuration are investigated by a subsonic panel method. Panel methods are best applicable to the lifting surfaces such as wings and airfoils. Source and doublets are used in the present code as a basic singularities of the panel technique. The panel method is first assessed by applying it to several benchmark problems for which other solutions and experimental data are available, such as a swept wing and wing body configuration. The prediction results are compared with experimental data and show good agreement in all cases considered. Finally, the method is applied to a T-50 aircraft configuration and excellent agreement with flight test data in lift coefficients is found.

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