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Volumn 2005, Issue , 2005, Pages 82-88

An electrostatically actuated valve for turbulent boundary layer control

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; ANEMOMETERS; BOUNDARY LAYERS; ELECTRODES; ELECTROSTATICS; VELOCITY MEASUREMENT;

EID: 33847306500     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICSENS.2005.1597642     Document Type: Conference Paper
Times cited : (13)

References (12)
  • 1
    • 0034825391 scopus 로고    scopus 로고
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    • T. Bewley, "Flow control : New challenges for a new renaissance," Progress in Aerospace Sciences, vol. 37, pp. 21-58, 2001.
    • (2001) Progress in Aerospace Sciences , vol.37 , pp. 21-58
    • Bewley, T.1
  • 3
    • 0013429561 scopus 로고    scopus 로고
    • Development of synthetic jet actuators for active flow control at nasa langley
    • Denver, Colorado
    • F.-J. Chen et al., "Development of synthetic jet actuators for active flow control at nasa langley," in Fluids 2000 - AIAA 2000-2405, Denver, Colorado, 2000.
    • (2000) Fluids 2000 - AIAA 2000-2405
    • Chen, F.-J.1
  • 4
    • 0030190678 scopus 로고    scopus 로고
    • Modern developments in flow control
    • M. G. el Hak, "Modern developments in flow control," Appl. Mech. Rev, vol. 49, pp. 365-379, 1996.
    • (1996) Appl. Mech. Rev , vol.49 , pp. 365-379
    • el Hak, M.G.1
  • 5
    • 1542786313 scopus 로고    scopus 로고
    • Micro-electro-mechanical systems (mems) and fluid flows
    • C. Ho and Y. C. Tai, "Micro-electro-mechanical systems (mems) and fluid flows," Ann. Rev. Fluid. Mech., vol. 30, pp. 602-609, 1998.
    • (1998) Ann. Rev. Fluid. Mech , vol.30 , pp. 602-609
    • Ho, C.1    Tai, Y.C.2
  • 6
    • 33847333258 scopus 로고    scopus 로고
    • Application of mems devices to delta air wing aircraft : From concept development to transonic flight test
    • Reno, Nevada, Jan
    • A. Huang et al., "Application of mems devices to delta air wing aircraft : from concept development to transonic flight test," in 39 th AIAA Aerospace Sciences - AIAA 2001-0124, Reno, Nevada, Jan. 2001.
    • (2001) 39 th AIAA Aerospace Sciences - AIAA 2001-0124
    • Huang, A.1
  • 7
    • 0033076350 scopus 로고    scopus 로고
    • Mems applications in turbulence and flow control
    • L. Lofdahl and M. G. el Hak, "Mems applications in turbulence and flow control," Progress in Aerospace Sciences, vol. 35, pp. 101-203, 1999.
    • (1999) Progress in Aerospace Sciences , vol.35 , pp. 101-203
    • Lofdahl, L.1    el Hak, M.G.2
  • 10
    • 0035472772 scopus 로고    scopus 로고
    • Adaptive wing and flow control technology
    • E. Stanewsky, "Adaptive wing and flow control technology," Progress in Aerospace Sciences, vol. 37, pp. 583-667, 2001.
    • (2001) Progress in Aerospace Sciences , vol.37 , pp. 583-667
    • Stanewsky, E.1
  • 12
    • 84897799637 scopus 로고    scopus 로고
    • Aeromems ii : A european research effort to develop mems based flow control technologies
    • C. Warsop, "Aeromems ii : A european research effort to develop mems based flow control technologies," in Proc. AIAA 2nd Flow Control Conference, 2004.
    • (2004) Proc. AIAA 2nd Flow Control Conference
    • Warsop, C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.