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Volumn , Issue , 2007, Pages

Design of a wind tunnel scale model of an adaptive wind turbine blade for active aerodynamic load control experiments

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AERODYNAMICS; ELECTRIC LOAD MANAGEMENT; GLASS CERAMICS; TURBINE COMPONENTS; WIND; WIND POWER; WIND TUNNELS; WIND TURBINES;

EID: 85076867523     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (13)

References (8)
  • 2
    • 0035250321 scopus 로고    scopus 로고
    • Wind tunnel testing of a Mach-scaled rotor model with trailing-edge flaps
    • Koratkar N.A. and Chopra I., "Wind tunnel testing of a Mach-scaled rotor model with trailing-edge flaps", Smart Materials and Structures, Vol. 10, pp1-14, 2001.
    • (2001) Smart Materials and Structures , vol.10 , pp. 1-14
    • Koratkar, N.A.1    Chopra, I.2
  • 3
    • 0035249462 scopus 로고    scopus 로고
    • Development of a piezoelectric actuator for trailing edge flap control of full scale rotor blades
    • Straub F.K., Ngo H.T., Anand V. and Domzalski D.B., "Development of a piezoelectric actuator for trailing edge flap control of full scale rotor blades", Smart Materials and Structures, Vol. 10, pp 25-34, 2001.
    • (2001) Smart Materials and Structures , vol.10 , pp. 25-34
    • Straub, F.K.1    Ngo, H.T.2    Anand, V.3    Domzalski, D.B.4
  • 4
    • 30744462098 scopus 로고    scopus 로고
    • Load reduction potential using airfoils with variable trailing edge geometry
    • Reno, Nevada, Jan. 10-13
    • Buhl T., Gaunaa M., Bak C., "Load Reduction Potential Using Airfoils With Variable Trailing Edge Geometry". 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 10-13, pp 1-18, 2005.
    • (2005) 43rd AIAA Aerospace Sciences Meeting and Exhibit , pp. 1-18
    • Buhl, T.1    Gaunaa, M.2    Bak, C.3
  • 6
    • 0028393040 scopus 로고
    • Unsteady lift of a flapped airfoil by indicial concepts
    • Leishman J.G., "Unsteady Lift of a Flapped Airfoil by Indicial Concepts". Journal of Aircraft, Vol. 31, No. 2, pp 288-297, 1994.
    • (1994) Journal of Aircraft , vol.31 , Issue.2 , pp. 288-297
    • Leishman, J.G.1
  • 7
    • 10444263069 scopus 로고    scopus 로고
    • Analysis of the manufactured shape of rectangular THUNDER-type actuators
    • Aimmanee S. and Hyer M.W., "Analysis of the manufactured shape of rectangular THUNDER-type actuators", Smart Materials and Structures, Vol. 13 pp 1389-1406, 2004.
    • (2004) Smart Materials and Structures , vol.13 , pp. 1389-1406
    • Aimmanee, S.1    Hyer, M.W.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.