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Volumn 52, Issue 3, 2007, Pages 254-262

Hover performance of a micro air vehicle: Rotors at low Reynolds number

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; FLOW VISUALIZATION; OPTIMIZATION; REYNOLDS NUMBER; WAKES;

EID: 34548131636     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/JAHS.52.254     Document Type: Article
Times cited : (130)

References (10)
  • 2
    • 34548112833 scopus 로고    scopus 로고
    • Schmitz, F. W., Aerodynamics of the Model Airplane (1941), Redstone Arsenal, N70-39001, RSIC-721, November 1967.
    • Schmitz, F. W., Aerodynamics of the Model Airplane (1941), Redstone Arsenal, N70-39001, RSIC-721, November 1967.
  • 3
    • 0004884644 scopus 로고    scopus 로고
    • Low Reynolds Number Airfoil Survey
    • 165803, I, 1981
    • Carmichael, B. H., "Low Reynolds Number Airfoil Survey," NASA Contractor Report 165803, Vol. I, 1981.
    • NASA Contractor Report
    • Carmichael, B.H.1
  • 4
    • 0002355156 scopus 로고    scopus 로고
    • Wind Tunnel Tests of Wings at Reynolds Numbers Below 70,000
    • Laitone, E. V., "Wind Tunnel Tests of Wings at Reynolds Numbers Below 70,000," Experiments in Fluids, Vol. 23, 1997, pp. 405-409.
    • (1997) Experiments in Fluids , vol.23 , pp. 405-409
    • Laitone, E.V.1
  • 5
    • 1542526163 scopus 로고    scopus 로고
    • Comparison of Wings Characteristics at an Ultralow Reynolds Number
    • March-April
    • Sunada, S., "Comparison of Wings Characteristics at an Ultralow Reynolds Number," Journal of Aircraft, Vol. 39, (2), March-April 2000, pp. 331-337.
    • (2000) Journal of Aircraft , vol.39 , Issue.2 , pp. 331-337
    • Sunada, S.1
  • 7
    • 34548115888 scopus 로고    scopus 로고
    • Leishman, J. G., Principles of Helicopter Aerodynamics, Cambridge University Press, New York, 2002, Chap. 2 and 3.
    • Leishman, J. G., Principles of Helicopter Aerodynamics, Cambridge University Press, New York, 2002, Chap. 2 and 3.
  • 8
    • 27844530483 scopus 로고
    • Tip Vortex Geometry of a Hovering Helicopter Rotor in Ground Effect
    • Boston, MA, May 22-24
    • Light, J. S., "Tip Vortex Geometry of a Hovering Helicopter Rotor in Ground Effect," American Helicopter Society 45th Annual Forum Proceedings, Boston, MA, May 22-24, 1989.
    • (1989) American Helicopter Society 45th Annual Forum Proceedings
    • Light, J.S.1
  • 9
    • 0037245097 scopus 로고    scopus 로고
    • Trailing Vortex Measurements in the Wake of a Hovering Rotor Blade with Various Tip Shapes
    • January
    • Martin, P. B., and Leishman, J. G., "Trailing Vortex Measurements in the Wake of a Hovering Rotor Blade with Various Tip Shapes," Journal of the American Helicopter Society, Vol. 48, (1), January 2003, pp. 39-52.
    • (2003) Journal of the American Helicopter Society , vol.48 , Issue.1 , pp. 39-52
    • Martin, P.B.1    Leishman, J.G.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.