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Volumn , Issue , 2004, Pages 2314-2326

Optimization of blowing and suction control on NACA 0012 airfoil using genetic algorithm

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; DRAG; GENETIC ALGORITHMS; LIFT; OPTIMIZATION; PROBLEM SOLVING; REYNOLDS NUMBER; VISCOSITY;

EID: 2942711527     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-225     Document Type: Conference Paper
Times cited : (14)

References (13)
  • 1
    • 0033930103 scopus 로고    scopus 로고
    • Real-coded adaptive range genetic algorithm and its application to aerodynamic design
    • Series A, February
    • Oyama., A., Obayashi, S., and Nakahashi, K., "Real-Coded Adaptive Range Genetic Algorithm and Its Application to Aerodynamic Design," JSME International Journal, Series A, Vol. 43, No. 2, pp. 124-129, February 2000.
    • (2000) JSME International Journal , vol.43 , Issue.2 , pp. 124-129
    • Oyama, A.1    Obayashi, S.2    Nakahashi, K.3
  • 2
    • 2942755018 scopus 로고    scopus 로고
    • Numerical study of blowing and suction control mechanism on NACA0012 airfoil
    • accepted for publication October
    • L. Huang, P.G. Huang, R.P. LeBeau and Th. Hauser, "Numerical Study of Blowing and Suction Control Mechanism on NACA0012 Airfoil", Journal of Aircraft, (accepted for publication October, 2003).
    • (2003) Journal of Aircraft
    • Huang, L.1    Huang, P.G.2    LeBeau, R.P.3    Hauser, Th.4
  • 3
    • 0003735261 scopus 로고    scopus 로고
    • Wiley-Interscience Publication, ISBN: 0-471-12741-8
    • Mitsuo Gen and Runwei Cheng, "Algorithms & Engineering Design", Wiley-Interscience Publication, ISBN: 0-471-12741-8, 1996
    • (1996) Algorithms & Engineering Design
    • Gen, M.1    Cheng, R.2
  • 7
    • 0141502492 scopus 로고    scopus 로고
    • Predictions of separated and transitional boundary layers under low-pressure turbine airfoil conditions using an intermittency transport equation
    • Jul.
    • Y. B. Suzen and P. G. Huang, "Predictions of Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions Using an Intermittency Transport Equation", Journal of Turbomachinery, Vol. 125, No.3, Jul. 2003, pp. 455-464
    • (2003) Journal of Turbomachinery , vol.125 , Issue.3 , pp. 455-464
    • Suzen, Y.B.1    Huang, P.G.2
  • 8
    • 0032155925 scopus 로고    scopus 로고
    • Post-stall flow control on an airfoil by local unsteady forcing
    • Jie-Zhi Wu, Xi-Yun Lu, Andrew G. Denny, Meng Fan and Jain-Ming Wu, "Post-stall Flow Control On An Airfoil By Local Unsteady Forcing", Journal of Fluid Mechanics, Vol. 371, 1998, pp. 21-58
    • (1998) Journal of Fluid Mechanics , vol.371 , pp. 21-58
    • Wu, J.-Z.1    Lu, X.-Y.2    Denny, A.G.3    Fan, M.4    Wu, J.-M.5
  • 10
    • 19544371289 scopus 로고
    • Aerodynamic characteristics of NACA0012 airfoil section at angles of attack from to
    • Chris C. Critzos, Harry H. Heyson and Robert W. Boswinkle Jr., "Aerodynamic Characteristics of NACA0012 Airfoil Section at Angles of Attack from to", NACA TN 3361, 1955
    • (1955) NACA TN , vol.3361
    • Critzos, C.C.1    Heyson, H.H.2    Boswinkle Jr., R.W.3
  • 11
    • 0038901774 scopus 로고
    • Airfoil section characteristics as affected by variations of the reynolds number
    • E. Jacobs, A. Shennan, "Airfoil Section Characteristics As Affected By Variations Of the Reynolds Number", NACA Report#586,231, 1937
    • (1937) NACA Report#586 , vol.586 , pp. 231
    • Jacobs, E.1    Shennan, A.2
  • 12
    • 0024665935 scopus 로고
    • A natural low-frequency oscillation of the flow over an airfoil near stalling conditions
    • K. B. M. Q. Zaman, D. J. McKinzie, and C. L. Rumsey, "A natural low-frequency oscillation of the flow over an airfoil near stalling conditions", Journal of Fluid Mechanics, Vol. 202, 1989, pp. 403-442.
    • (1989) Journal of Fluid Mechanics , vol.202 , pp. 403-442
    • Zaman, K.B.M.Q.1    McKinzie, D.J.2    Rumsey, C.L.3
  • 13
    • 77958452366 scopus 로고
    • Section characteristics of a 10.5-percent thick airfoil with area suction as affected by chordwise distribution of permeability
    • Ames Aeronautical Laboratory, Moffett Field, CA, Dec.
    • Robert E. Dannenberg and James A. Weiberg, "Section Characteristics Of A 10.5-Percent Thick Airfoil With Area Suction As Affected By Chordwise Distribution Of Permeability", NASA Technical Note 2847, Ames Aeronautical Laboratory, Moffett Field, CA, Dec. 1952
    • (1952) NASA Technical Note , vol.2847
    • Dannenberg, R.E.1    Weiberg, J.A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.