메뉴 건너뛰기




Volumn 319, Issue 5867, 2008, Pages 1250-1253

Leading-edge vortex improves lift in slow-flying bats

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BAT; FLIGHT; FLY; IMAGE; NECTAR;

EID: 40049091461     PISSN: 00368075     EISSN: 10959203     Source Type: Journal    
DOI: 10.1126/science.1153019     Document Type: Article
Times cited : (321)

References (33)
  • 2
    • 40049087536 scopus 로고    scopus 로고
    • Quasi-steady-state wing theory assumes that the forces on a moving wing are equivalent to the sum of the forces on a fixed wing over a sequence of attitudes that track the wing motion. This model neglects acceleration forces and unsteady aerodynamic effects
    • Quasi-steady-state wing theory assumes that the forces on a moving wing are equivalent to the sum of the forces on a fixed wing over a sequence of attitudes that track the wing motion. This model neglects acceleration forces and unsteady aerodynamic effects.
  • 8
    • 0003799829 scopus 로고
    • Princeton Univ. Press, Princeton, NJ
    • S. Vogel, Life in Moving Fluids (Princeton Univ. Press, Princeton, NJ, 1994).
    • (1994) Life in Moving Fluids
    • Vogel, S.1
  • 18
    • 0001425771 scopus 로고
    • T. Y.-T. Wu, C. J. Brokaw, C. Brennen, Eds, Plenum, New York
    • U. M. Norberg, in Swimming and Flying in Nature, vol. 2, T. Y.-T. Wu, C. J. Brokaw, C. Brennen, Eds. (Plenum, New York, 1975), pp. 869-881.
    • (1975) Swimming and Flying in Nature , vol.2 , pp. 869-881
    • Norberg, U.M.1
  • 22
    • 40049095291 scopus 로고    scopus 로고
    • See supporting material on Science Online.
    • See supporting material on Science Online.
  • 23
    • 40049096758 scopus 로고    scopus 로고
    • 5) where the aerodynamics are notoriously hard to predict and control.
    • 5) where the aerodynamics are notoriously hard to predict and control.
  • 24
    • 40049093870 scopus 로고    scopus 로고
    • St = fA/U∞ (f is wingbeat frequency and A is the tip-to-tip vertical excursion of the wing tip). St is proportional to the ratio of the average wingbeat velocity to the steady forward speed and is an indication of the unsteadiness and efficiency of vortex generation.
    • St = fA/U∞ (f is wingbeat frequency and A is the tip-to-tip vertical excursion of the wing tip). St is proportional to the ratio of the average wingbeat velocity to the steady forward speed and is an indication of the unsteadiness and efficiency of vortex generation.
  • 25
    • 40049103431 scopus 로고    scopus 로고
    • For an incompressible fluid, the divergence in a planar velocity field is related to the change in out-of-plane flow velocity. When the divergence is positive, the fluid works as a fluid source in the planar velocity field, decreasing the out-of-plane velocity. When it is negative, it is a fluid sink, which increases the out-of-plane velocity
    • For an incompressible fluid, the divergence in a planar velocity field is related to the change in out-of-plane flow velocity. When the divergence is positive, the fluid works as a fluid source in the planar velocity field, decreasing the out-of-plane velocity. When it is negative, it is a fluid sink, which increases the out-of-plane velocity.
  • 33
    • 40049111820 scopus 로고    scopus 로고
    • We thank R. von Busse and Y. Winter for their support. This work was supported by grants from the Swedish Research Council, the Swedish Foundation for International Cooperation in Research and Higher Education, the Knut and Alice Wallenberg Foundation, the Crafoord Foundation, the Magnus Bergvall Foundation, and the Royal Physiographical Society
    • We thank R. von Busse and Y. Winter for their support. This work was supported by grants from the Swedish Research Council, the Swedish Foundation for International Cooperation in Research and Higher Education, the Knut and Alice Wallenberg Foundation, the Crafoord Foundation, the Magnus Bergvall Foundation, and the Royal Physiographical Society.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.