Journal of computational fluids engineering (한국전산유체공학회지)

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
권호 표지

AERODYNAMIC DESIGN OPTIMIZATION OF ROTOR AIRFOIL WITH MULTIPLE CONSTRAINTS

다중제약조건을 갖는 로터익형의 공력 최적 설계

  • 이세민 (건국대학교 대학원 항공우주정보시스템공학과) ;
  • 사정환 (건국대학교 대학원 항공우주정보시스템공학과) ;
  • 전상언 (건국대학교 대학원 항공우주정보시스템공학과) ;
  • 김창주 (건국대학교 항공우주정보시스템공학과) ;
  • 박수형 (건국대학교 항공우주정보시스템공학과) ;
  • 정기훈 (한국항공우주연구원)
  • Received : 2010.05.06
  • Accepted : 2010.06.25
  • Published : 2010.06.30
Download PDF
⟨ Previous Next ⟩

Abstract

Aerodynamic design optimization of rotor airfoil has been performed with advanced design method for improved aerodynamic characteristics of ONERA airfoils. A multiple response surface method is used to consider various requirements in rotor airfoil design. Shape functions for mean camber line are proposed to extend possible design domain. Numerical simulations are performed using KFLOW, a Navier-Stokes solver with shear stress transport turbulence model. The present design method provides favorable configurations for the high performance rotor airfoil. Resulting optimized airfoils give better aerodynamic performance than the baseline airfoils.

Keywords

References

  1. 2000, Jones, B.R., Crossley, W.A. and Lyrintzis, A.S., "Aerodynamic and Aeroacoustic Optimization of Rotorcraft Airfoils via a Parallel Genetic Algorithm," Journal of Aircraft, Vol.37, No.6, pp.1088-1096. https://doi.org/10.2514/2.2717
  2. 1978, Dadone, L.U., "Design and Analytical Study of a Rotor Airfoil," NASA Contractor Report, NASA CR-2988.
  3. 2009, 사정환, 박수형, 김창주, 윤철용, 김승호, 김상호, 유영훈, "로터 블레이드 OA 익형의 공력 최적 설계," 한국전산유체공학회지, 제14권, 제2호, pp.25-31.
  4. 2002, Myers, R.H. and Montgomery, D.C., Response Surface Methodology, John Wiley and Sons, New York, NY, USA.
  5. 1978, Hicks, R.M. and Henne, P.A., "Wing design by numerical optimization," Journal of Aircraft, Vol.15, No7, pp.407-412. https://doi.org/10.2514/3.58379
  6. 1990, Batina, J.T., Robinson, B.A. and Yang, H.T., "Aeroelastic analysis of wings using the Euler equations with a deforming mesh," NASA Technical Memorandum, NASA TM-102733.
  7. 2004, Park, S.H. and Kwon, J.H., "Implementation of $\kappa$-$\omega$ Turbulence Models in an Implicit Multigrid Method," AIAA journal, Vol.42, No.7, pp.1348-1357. https://doi.org/10.2514/1.2461
  8. 1990, Vuillet, A., "Rotor and Blade Aerodynamic Design," AGARD-FDP Special course on Aerodynamics of Rotorcraft, VKI, Brussels, Belgium.
  9. 2002, Bousman, W.G., "Airfoil Design and Rotorcraft Performance," 58th AHS Forum, Montreal, Canada.
  10. 1969, Wortmann, F.X. and Drees, J.M., "Design of Airfoils for Rotors," CAL/AVLABS 1969 Symposium on Aerodynamics of Rotary Wing and VTOL Aircraft.