e-science 기반의 항공우주분야 교육, 연구용 공력 최적 설계 프레임워크를 활용한 에어포일의 역설계 연구A STUDY ON INVERSE DESIGN OF AIRFOIL USING e-Science BASED AERODYNAMICS DESIGN OPTIMIZATION FRAMEWORK

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 319
  • Download : 159
Recently, with advanced computational performance, numerical design optimization including CFD has been developed in aerospace engineering. However it could hardly find the design optimization softwares and contents of which educational purposes in aerospace engineering. In this study, inverse shape design is developed for steady, two dimensional inviscid and compressible flow over airfoils using aerodynamic design optimization framework for an airfoil based on EDISON_CFD(Education-research through Simulation On the Net for Computational Fluid Dynamics). Design optimization is performed for drag minimization in transonic flow. Two target pressure distributions are RAE2822 known as transonic airfoil and previously designed airfoil for drag minimized from NACA0012 airfoil. Both result showed that shape, lift coefficient, and drag coefficient of baseline airfoil got closer to those of target airfoil. From a result, contents of design optimization framework could be expected to help in the lecture.
Publisher
한국전산유체공학회
Issue Date
2012-05-25
Language
Korean
Citation

한국전산유체공학회 2012년도 춘계학술대회

URI
http://hdl.handle.net/10203/172280
Appears in Collection
ME-Conference Papers(학술회의논문)

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0