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Volumn , Issue , 2001, Pages

Induced-shear piezoelectric actuators for rotor blade trailing edge flaps and active tips

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FINITE ELEMENT METHOD; LOAD TESTING; PIEZOELECTRICITY; VIBRATION ANALYSIS;

EID: 85067322415     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1559     Document Type: Conference Paper
Times cited : (6)

References (37)
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  • 8
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    • February
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  • 10
    • 0032665192 scopus 로고    scopus 로고
    • Trailing Edge Flap Activated by a Piezo Induced Bending Torsion Coupled Beam
    • January
    • Bernhard, A. and Chopra, I., 'Trailing Edge Flap Activated by a Piezo Induced Bending Torsion Coupled Beam, Journal of the American Helicopter Society, Vol. 44, January 1999, pp. 1-15.
    • (1999) Journal of the American Helicopter Society , vol.44 , pp. 1-15
    • Bernhard, A.1    Chopra, I.2
  • 20
    • 85086491914 scopus 로고    scopus 로고
    • Structural Dynamics, and Materials Conference, Atlanta, April
    • a AIAA Structures, Structural Dynamics, and Materials Conference, Atlanta, April 2000.
    • (2000) a AIAA Structures
    • Prechtl, E.F.1    Hall, S.R.2
  • 29
    • 0000913562 scopus 로고    scopus 로고
    • Piezoelectric Actuator Generating Torsional Displacement from Piezoelectric d 15 Shear Response
    • May
    • Glazounov, A.E., Zhang, Q.M., and Kim, C, Piezoelectric Actuator Generating Torsional Displacement from Piezoelectric d15 Shear Response, Applied Physics Letters, Vol. 72, No. 20, May 1998, pp. 2526-2528.
    • (1998) Applied Physics Letters , vol.72 , Issue.20 , pp. 2526-2528
    • Glazounov, A.E.1    Zhang, Q.M.2    Kim, C.3
  • 33
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    • General Theory of Aerodynamic Instability and the Mechanism of Flutter
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    • Theodorsen, T.1
  • 34
    • 0030247268 scopus 로고    scopus 로고
    • Unsteady Aerodynamics of a Flapped Airfoil in Subsonic Flow by Indicial Concepts
    • September-October
    • Hariharan, N. and Leishman, J.G., Unsteady Aerodynamics of a Flapped Airfoil in Subsonic Flow by Indicial Concepts, Journal of Aircraft, Vol. 33, No. 5, September-October 1996, pp. 855-868.
    • (1996) Journal of Aircraft , vol.33 , Issue.5 , pp. 855-868
    • Hariharan, N.1    Leishman, J.G.2
  • 36
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    • Piezo-Kinetics Inc., Bellefonte, PA
    • Piezo-Kinetics Inc., Bellefonte, PA


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.