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Volumn 1, Issue , 2007, Pages 22-29

Load alleviation through adaptive trailing edge control surfaces: ADAPWING overview

Author keywords

Load alleviation; Trailing edge flaps; Wind tunnel test

Indexed keywords

LOAD ALLEVIATION; LOAD REDUCTION POTENTIAL; NUMERICAL AND EXPERIMENTAL STUDY; NUMERICAL INVESTIGATIONS; TRAILING EDGE FLAPS; TRAILING EDGE GEOMETRIES; TRAILING-EDGE CONTROL SURFACES; WIND TUNNEL TESTS;

EID: 84875305001     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (20)

References (13)
  • 1
    • 13244273564 scopus 로고    scopus 로고
    • Active load reduction using individual pitch, based on local blade flow measurements
    • Larsen, T.J., Madsen, H.Aa. and Thomsen, K. "Active Load Reduction Using Individual Pitch, Based on Local Blade Flow Measurements", Wind Energy, Vol. 8 issue 1, p. 67-80, 2004.
    • (2004) Wind Energy , vol.8 , Issue.1 , pp. 67-80
    • Larsen, T.J.1    Madsen, H.Aa.2    Thomsen, K.3
  • 2
    • 14344265839 scopus 로고    scopus 로고
    • Developments in individual blade pitch contro
    • Bossanyi, E.A., "Developments in Individual Blade Pitch Contro", Wind Energy, Vol. 6 issue 3, p. 229-244, 2003.
    • (2003) Wind Energy , vol.6 , Issue.3 , pp. 229-244
    • Bossanyi, E.A.1
  • 4
    • 0003927402 scopus 로고
    • General theory of aerodynamical instability and the mechanism of flutter
    • Theodorsen, T., "General Theory of Aerodynamical Instability and the Mechanism of Flutter". NACA Report 496, Vol.496, 1935.
    • (1935) NACA Report 496 , vol.496
    • Theodorsen, T.1
  • 7
    • 27744477904 scopus 로고    scopus 로고
    • Potential load reduction using airfoils with variable trailing edge geometry
    • Buhl, T., Gaunaa, M. and Bak, C., "Potential Load Reduction Using Airfoils with Variable Trailing Edge Geometry", Journal of Solar Energy Engineering, Vol. 127, pp. 503-516, 2005.
    • (2005) Journal of Solar Energy Engineering , vol.127 , pp. 503-516
    • Buhl, T.1    Gaunaa, M.2    Bak, C.3
  • 9
    • 0028393040 scopus 로고
    • Unsteady lift of a flapped airfoil by indicial concept's
    • Leishman, J.G., "Unsteady Lift of a Flapped Airfoil by Indicial Concept's, Journal of Aircraft, vol. 31(2), pp. 288-297, 1994.
    • (1994) Journal of Aircraft , vol.31 , Issue.2 , pp. 288-297
    • Leishman, J.G.1
  • 10
    • 0030247268 scopus 로고    scopus 로고
    • Unsteady aerodynamics of a flapped airfoil in subsonic flow by indicial concepts
    • Hariharan, N. and Leishman, J.G. "Unsteady Aerodynamics of a Flapped Airfoil in Subsonic Flow by Indicial Concepts", Journal of Aircraft, vol. 33(5), pp. 855-868, 1996.
    • (1996) Journal of Aircraft , vol.33 , Issue.5 , pp. 855-868
    • Hariharan, N.1    Leishman, J.G.2
  • 11
    • 0018434779 scopus 로고
    • The effect of chordwise flexibility on the lift of a rapidly accelerated air- foil
    • Katz, J. and Weihs, D., "The Effect of Chordwise Flexibility on the Lift of a Rapidly Accelerated Air- foil, Aeronautical Quarterly, vol.30, pp. 360-370, 1979.
    • (1979) Aeronautical Quarterly , vol.30 , pp. 360-370
    • Katz, J.1    Weihs, D.2
  • 12
    • 0032685252 scopus 로고    scopus 로고
    • Ex- preimental and numerical investigations on steady and unsteady behaviour of a rotor airfoil with a piezoelectric trailing edge flap
    • Montreal, Canada
    • van der Wall, B.G. and Geissler, W., "Ex- preimental and Numerical Investigations on Steady and Unsteady Behaviour of a Rotor Airfoil with a Piezoelectric Trailing Edge Flap", 55th American Helicopter Society Forum, Montreal, Canada, 1999.
    • (1999) 55th American Helicopter Society Forum
    • Van Der Wall, B.G.1    Geissler, W.2
  • 13
    • 34250844923 scopus 로고    scopus 로고
    • Wind tunnel test on wind turbine airfoil with adaptive trailing edge geometty
    • Reno, NV (US), 8-11 Jan, (American Institute of Aeronautics and Astronautics, Reston, VA, 2007) (AIAA-2007-1016
    • Bak, C., Gaunaa, M., Andersen, P.B., Buhl, T., Hansen, P., Clemmensen, K. and Mailer, R., Wind tunnel test on wind turbine airfoil with adaptive trailing edge geometty. 45. AIAA aerospace sciences meeting and exhibit, Reno, NV (US), 8-11 Jan 2007. (American Institute of Aeronautics and Astronautics, Reston, VA, 2007) (AIAA-2007-1016).
    • (2007) AIAA Aerospace Sciences Meeting and Exhibit , pp. 45
    • Bak, C.1    Gaunaa, M.2    Andersen, P.B.3    Buhl, T.4    Hansen, P.5    Clemmensen, K.6    Mailer, R.7


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.