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Volumn 44, Issue 4, 2007, Pages 1245-1257

Aerodynamic loading for an airfoil with an oscillating gurney flap

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; FLOW CONTROL; METHOD OF MOMENTS; NASA; NAVIER STOKES EQUATIONS;

EID: 34548351754     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.26440     Document Type: Conference Paper
Times cited : (61)

References (9)
  • 1
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    • Design of Subsonic Airfoil for High Lift
    • Liebeck, R. H., "Design of Subsonic Airfoil for High Lift," Journal of Aircraft, Vol. 15, No. 9, 1978, pp. 547-561.
    • (1978) Journal of Aircraft , vol.15 , Issue.9 , pp. 547-561
    • Liebeck, R.H.1
  • 2
    • 0033894883 scopus 로고    scopus 로고
    • Aerodynamics of Gumey Flaps on a Single-Element High-Lift Wing
    • Jeffrey, D., Zhang, X., and Hurst, D. W., "Aerodynamics of Gumey Flaps on a Single-Element High-Lift Wing," Journal of Aircraft, Vol. 37, No. 2,2000, pp. 295-301.
    • (2000) Journal of Aircraft , vol.37 , Issue.2 , pp. 295-301
    • Jeffrey, D.1    Zhang, X.2    Hurst, D.W.3
  • 3
    • 0032663158 scopus 로고    scopus 로고
    • Gurney Flap Experiments on Airfoil and Wings
    • Van Dam, C. P., Yen D. T. and Vijhen, P. M. H. W., "Gurney Flap Experiments on Airfoil and Wings," Journal of Aircraft, Vol. 36, No. 2, 1999, pp. 484-486.
    • (1999) Journal of Aircraft , vol.36 , Issue.2 , pp. 484-486
    • Van Dam, C.P.1    Yen, D.T.2    Vijhen, P.M.H.W.3
  • 4
    • 0028427388 scopus 로고
    • Lift Enhancement of an Airfoil Using a Gurney Flap and Vortex Generators
    • Storms, B. L., and Jang, C. S., "Lift Enhancement of an Airfoil Using a Gurney Flap and Vortex Generators," Journal of Aircraft, Vol. 31, No. 3, 1994, pp. 542-547.
    • (1994) Journal of Aircraft , vol.31 , Issue.3 , pp. 542-547
    • Storms, B.L.1    Jang, C.S.2
  • 5
    • 0035334814 scopus 로고    scopus 로고
    • Dynamic Stall Control by Periodic Excitation, Part 1: NACA0015 Parametric Study
    • Greenblatt, D., and Wygnanski, I., "Dynamic Stall Control by Periodic Excitation, Part 1: NACA0015 Parametric Study," Journal of Aircraft, Vol. 38, No. 3, 2001, pp. 430-438.
    • (2001) Journal of Aircraft , vol.38 , Issue.3 , pp. 430-438
    • Greenblatt, D.1    Wygnanski, I.2
  • 6
    • 0035083572 scopus 로고    scopus 로고
    • Dynamic Stall Control by Intermittent Periodic Excitation
    • Greenblatt, D., Neuburger, D., and Wygnanski, I.. "Dynamic Stall Control by Intermittent Periodic Excitation, "Journal of Aircraft, Vol. 38, No. 1, 2001, pp. 188-190.
    • (2001) Journal of Aircraft , vol.38 , Issue.1 , pp. 188-190
    • Greenblatt, D.1    Neuburger, D.2    Wygnanski, I.3
  • 7
    • 33846078336 scopus 로고    scopus 로고
    • Aerodynamic Flow Control of An Airfoil with Small Trailing Edge Strips
    • Tang, Deman, and Dowell, E. H., "Aerodynamic Flow Control of An Airfoil with Small Trailing Edge Strips," Journal of Aircraft, Vol. 43, No. 6, 2006, pp. 1854-1866.
    • (2006) Journal of Aircraft , vol.43 , Issue.6 , pp. 1854-1866
    • Tang, D.1    Dowell, E.H.2
  • 8
    • 33646386943 scopus 로고    scopus 로고
    • Oscillating Wing Loadings with Small Trailing-Edge Strips
    • Mar.-Apr
    • Gerontakos, P., and Lee, T., "Oscillating Wing Loadings with Small Trailing-Edge Strips," Journal of Aircraft, Vol. 43, No. 2, Mar.-Apr., 2006, pp. 428-436.
    • (2006) Journal of Aircraft , vol.43 , Issue.2 , pp. 428-436
    • Gerontakos, P.1    Lee, T.2
  • 9
    • 33847718305 scopus 로고    scopus 로고
    • Wake Vortex Control Using Static Segmented Gurney Flaps
    • Matalanis, C. G., and Eaton, J. K., "Wake Vortex Control Using Static Segmented Gurney Flaps," AIAA Journal, Vol. 45, No. 2, 2007, pp. 321-328.
    • (2007) AIAA Journal , vol.45 , Issue.2 , pp. 321-328
    • Matalanis, C.G.1    Eaton, J.K.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.