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Volumn , Issue , 2000, Pages

A computational investigation of dynamic stall alleviation using leading edge deformation

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Indexed keywords


EID: 84894453199     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (19)
  • 3
    • 84894413267 scopus 로고    scopus 로고
    • Post-Stall Lift Enhancement on an Airfoil by Local Unsteady Control.Mode Competition and Vortex Dynamics
    • AIAA Paper 97-2064
    • Wu, J.Z., Lu, X.Y., and Wu, J.M. Post-Stall Lift Enhancement on an Airfoil by Local Unsteady Control. Part 2: Mode Competition and Vortex Dynamics. AIAA Paper 97-2064, 1997.
    • Part 2: Mode Competition and Vortex Dynamics
    • Wu, J.Z.1    Lu, X.Y.2    Wu, J.M.3
  • 12
    • 0027591735 scopus 로고
    • TURNS: A Free Wake Euler/ Navier-Stokes Numerical Method for Helicopter Rotors
    • May
    • Srinivasan, G.R. and Baeder, ID., TURNS: A Free Wake Euler/ Navier-Stokes Numerical Method for Helicopter Rotors, AIAA Journal, Vol. 31 No. 5, May 1993, pp. 959-962.
    • (1993) AIAA Journal , vol.31 , Issue.5 , pp. 959-962
    • Srinivasan, G.R.1    Baeder, I.D.2
  • 14
    • 2942757053 scopus 로고
    • Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes
    • Roe, P.L., Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes, Journal of Computational Physics, Vol. 43, No. 3., 1981. pp. 357-372.
    • (1981) Journal of Computational Physics , vol.43 , Issue.3 , pp. 357-372
    • Roe, P.L.1
  • 15
    • 0000104174 scopus 로고
    • Thin Layer Approximation and Algebraic Model For Separated Turbulent Flows
    • Baldwin, B.S and Lomax, H. Thin Layer Approximation and Algebraic Model For Separated Turbulent Flows. AIAA 78-257, 1978.
    • (1978) AIAA , pp. 78-257
    • Baldwin, B.S.1    Lomax, H.2
  • 16
    • 84894424900 scopus 로고
    • Compendium of Unsteady Aerodynamic Measurements, Advisory Group For Aerospace Research and Development
    • North Atlantic Treaty Organization, August
    • Compendium of Unsteady Aerodynamic Measurements, Advisory Group For Aerospace Research and Development. North Atlantic Treaty Organization. AGARD-R-702. August 1982.
    • (1982) AGARD-R-702
  • 17
    • 84894419769 scopus 로고    scopus 로고
    • Computations of Unsteady Separating Flows over an Oscillating Airfoil
    • Paper
    • Ko, S. and McCrosky, WJ. Computations of Unsteady Separating Flows over an Oscillating Airfoil. AIAA Paper 95-0312.
    • AIAA , pp. 95-0312
    • Ko, S.1    McCrosky, W.J.2
  • 19
    • 0004309674 scopus 로고    scopus 로고
    • Dynamic Stall of an Oscillating Wing Part 2: Evaluation of Turbulence Models
    • Paper
    • Srinivasan, G.R., Ekaterinaris, J.A., and McCroskey W.J. Dynamic Stall of an Oscillating Wing Part 2: Evaluation of Turbulence Models. AIAA Paper 93-3403.
    • AIAA , pp. 93-3403
    • Srinivasan, G.R.1    Ekaterinaris, J.A.2    McCroskey, W.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.