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Volumn 41, Issue 5, 2004, Pages 1005-1013

Numerical study of blowing and suction control mechanism on NACA0012 airfoil

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL GEOMETRY; COMPUTER SIMULATION; JETS; PARAMETER ESTIMATION; PRESSURE EFFECTS; SHEAR STRESS; SOFTWARE PROTOTYPING; TURBULENCE;

EID: 7544251830     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.2255     Document Type: Article
Times cited : (150)

References (23)
  • 1
    • 7544230902 scopus 로고
    • A brief history of British research on boundary layer control for high lift
    • Pergamon, New York
    • Williams, J., "A Brief History of British Research on Boundary Layer Control for High Lift," Boundary Layer and Flow Control, Pergamon, New York, 1961, pp. 74-103.
    • (1961) Boundary Layer and Flow Control , pp. 74-103
    • Williams, J.1
  • 2
    • 0343184729 scopus 로고
    • History of research on boundary layer control for low drag in U.K.
    • Pergamon, New York
    • Head, M. R., "History of Research on Boundary Layer Control for Low Drag in U.K.," Boundary Layer and Flow Control, Pergamon, New York, 1961, pp. 104-121.
    • (1961) Boundary Layer and Flow Control , pp. 104-121
    • Head, M.R.1
  • 3
    • 0343184730 scopus 로고
    • The history of boundary layer control research in the United States of America
    • Pergamon, New York
    • Flatt, J. "The History of Boundary Layer Control Research in the United States of America," Boundary Layer and Flow Control, Pergamon, New York, 1961, pp. 122-143.
    • (1961) Boundary Layer and Flow Control , pp. 122-143
    • Flatt, J.1
  • 4
    • 77958452366 scopus 로고
    • Section characteristics of a 10.5-percent thick airfoil with area suction as affected by chordwise distribution of permeability
    • Dec.
    • Dannenberg, R. E., and Weiberg, J. A., "Section Characteristics of a 10.5-Percent Thick Airfoil with Area Suction as Affected by Chordwise Distribution of Permeability," NASA TN 2847, Dec. 1952.
    • (1952) NASA TN , vol.2847
    • Dannenberg, R.E.1    Weiberg, J.A.2
  • 5
    • 85055412641 scopus 로고
    • Section characteristics of an NACA 0006 airfoil with area suction near the leading edge
    • Sept.
    • Weiberg, J. A., and Dannenberg, R. E., "Section Characteristics of an NACA 0006 Airfoil with Area Suction Near the Leading Edge," NASA TN 3285, Sept. 1954.
    • (1954) NASA TN , vol.3285
    • Weiberg, J.A.1    Dannenberg, R.E.2
  • 6
    • 7544225634 scopus 로고
    • Theory of boundary layer suction to prevent separation
    • Pergamon, New York
    • Wuest, W., "Theory of Boundary Layer Suction to Prevent Separation," Boundary Layer and Flow Control, Pergamon, New York, 1961, pp. 196-208.
    • (1961) Boundary Layer and Flow Control , pp. 196-208
    • Wuest, W.1
  • 7
    • 11644312718 scopus 로고    scopus 로고
    • The formation and evolution of synthetic jets
    • Smith, B. L., and Glezer, A., "The Formation and Evolution of Synthetic Jets," Physics of Fluids, Vol. 10, No. 9, 1998, pp. 2281-2297.
    • (1998) Physics of Fluids , vol.10 , Issue.9 , pp. 2281-2297
    • Smith, B.L.1    Glezer, A.2
  • 8
    • 0033169627 scopus 로고    scopus 로고
    • Numerical investigation of synthetic-jet flowfields
    • Rizzetta, D. P., Visbal, M. R., and Stanek, M. J., "Numerical Investigation of Synthetic-Jet Flowfields," AIAA Journal, Vol 37, No. 8, 1999, pp. 919-927.
    • (1999) AIAA Journal , vol.37 , Issue.8 , pp. 919-927
    • Rizzetta, D.P.1    Visbal, M.R.2    Stanek, M.J.3
  • 9
    • 0032155925 scopus 로고    scopus 로고
    • Post-stall flow control on an airfoil by local unsteady forcing
    • Wu, J.-Z., Lu, X.-Y., Denny, A. G., Fan, M., and Wu, J.-M., "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
    • 7544222703 scopus 로고    scopus 로고
    • Synthetic jets influence on NACA0012 airfoil at high angle of attacks
    • Aug.
    • Nae, C., "Synthetic Jets Influence on NACA0012 Airfoil at High Angle of Attacks," AIAA Paper 98-4523, Aug. 1998.
    • (1998) AIAA Paper , vol.98 , Issue.4523
    • Nae, C.1
  • 12
    • 7544247381 scopus 로고    scopus 로고
    • Numerical simulation of wake passing on turbine cascades
    • Jan.
    • Suzen, Y. B., and Huang, P. G., "Numerical Simulation of Wake Passing on Turbine Cascades," AIAA Paper 2003-1256, Jan. 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.1256
    • Suzen, Y.B.1    Huang, P.G.2
  • 13
    • 34548754140 scopus 로고    scopus 로고
    • A comprehensive CFD study of transitional flows in low-pressure turbines under a wide range of operation conditions
    • June
    • Suzen, Y. B., Huang, P. G., Volino, R. J., Corke, T. C., Thomas, F. O., Huang, J., Lake, J. P., and King, P. I., "A Comprehensive CFD Study of Transitional Flows in Low-Pressure Turbines Under a Wide Range of Operation Conditions," AIAA Paper 2003-3591, June 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.3591
    • Suzen, Y.B.1    Huang, P.G.2    Volino, R.J.3    Corke, T.C.4    Thomas, F.O.5    Huang, J.6    Lake, J.P.7    King, P.I.8
  • 14
    • 0141502492 scopus 로고    scopus 로고
    • Predictions of separated and transitional boundary layers under low-pressure turbine airfoil conditions using an intermittency transport equation
    • Suzen, Y. B., and Huang, P. G., "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, 2003, pp. 455-464.
    • (2003) Journal of Turbomachinery , vol.125 , Issue.3 , pp. 455-464
    • Suzen, Y.B.1    Huang, P.G.2
  • 15
    • 0028486598 scopus 로고
    • Two-equation eddy-viscosity turbulence models for engineering applications
    • Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA Journal, Vol. 32, No. 8, 1994, pp. 1598-1605.
    • (1994) AIAA Journal , vol.32 , Issue.8 , pp. 1598-1605
    • Menter, F.R.1
  • 17
    • 0013442405 scopus 로고
    • Aerodynamic characteristics of seven airfoil sections through 180 degrees angle of attack for use in aerodynamic analysis of vertical axis wind turbines
    • Albuquerque, NM, March
    • Sheldahl, R. E., and Klimas, P. C., "Aerodynamic Characteristics of Seven Airfoil Sections Through 180 Degrees Angle of Attack for use in Aerodynamic Analysis of Vertical Axis Wind Turbines," Sandia National Labs., Rept. SAND80-2114, Albuquerque, NM, March 1981.
    • (1981) Sandia National Labs., Rept. , vol.SAND80-2114
    • Sheldahl, R.E.1    Klimas, P.C.2
  • 18
    • 1242313131 scopus 로고
    • Aerodynamic characteristics of NACA0012 airfoil section at angles of attack from 0° to 180°
    • Jan.
    • Critzos, C. C., Heyson, H. H., and Boswinkle, R. W., Jr., "Aerodynamic Characteristics of NACA0012 Airfoil Section at Angles of Attack from 0° to 180°," NACA TN 3361, Jan. 1995.
    • (1995) NACA TN , vol.3361
    • Critzos, C.C.1    Heyson, H.H.2    Boswinkle Jr., R.W.3
  • 19
    • 0038901774 scopus 로고
    • Airfoil section characteristics as affected by variations of the reynolds number
    • Jacobs, E., and Sherman, A., "Airfoil Section Characteristics as Affected by Variations of the Reynolds Number," NACA Rept. 586,231, 1937.
    • (1937) NACA Rept. , vol.586 , pp. 231
    • Jacobs, E.1    Sherman, A.2
  • 20
    • 0024665935 scopus 로고
    • A natural low-frequency oscillation of the flow over an airfoil near stalling conditions
    • Zaman, K. B. M. Q., McKinzie, D. J., and Rumsey, C. L., "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
  • 21
    • 0037543142 scopus 로고
    • A critical assessment of wind tunnel results for the NACA0012 airfoil
    • Oct.
    • McCroskey, W. J., "A Critical Assessment of Wind Tunnel Results for the NACA0012 Airfoil," NASA TM 100019, Oct. 1987.
    • (1987) NASA TM 100019
    • McCroskey, W.J.1
  • 22
    • 2342456915 scopus 로고    scopus 로고
    • Compact, high-power synthetic jet actuators for flow separation control
    • Jan.
    • Gilarranz, J. L., and Rediniotis, O. K., "Compact, High-Power Synthetic Jet Actuators for Flow Separation Control," AIAA Paper 2001-0737, Jan. 2001.
    • (2001) AIAA Paper , vol.2001 , Issue.737
    • Gilarranz, J.L.1    Rediniotis, O.K.2
  • 23
    • 0032184076 scopus 로고    scopus 로고
    • Effects of zero-mass synthetic jets on the aerodynamics of the NACA-0012 airfoil
    • Oct.
    • Hassan, A., and Janakiram, R. D., "Effects of Zero-Mass Synthetic Jets on the Aerodynamics of the NACA-0012 Airfoil," Journal of the American Helicopter Society, Vol. 43, No. 4, Oct. 1998.
    • (1998) Journal of the American Helicopter Society , vol.43 , Issue.4
    • Hassan, A.1    Janakiram, R.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.