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  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Journal of comparative physiology 165 (1995), S. 255-267 
    ISSN: 1432-136X
    Keywords: Avian osmoregulation ; Salt gland ; Saltwater adaptation ; Maximum secretion capacity ; Eider duck (Somateria mollissima)
    Source: Springer Online Journal Archives 1860-2000
    Topics: Biology , Medicine
    Notes: Abstract The function of the supra-orbital salt gland was studied in the common eider duck (Somateria mollissima). The maximum salt-secreting capacity was determined in (1) wild ducks which had been living in a marine environment, (2) ducks reared in captivity on fresh water, and (3) ducks from group 2 adapted to salt water. The maximum secreting capacity was found by infusing a solution of NaCl (1000 mosmol·kg-1) at increasing rates, from 0.691 to 1.671 mosmol·min-1. Freshwater-adapted ducks secreted at a maximum rate of 0.785 mosmol·min-1 (1500 mosmol·kg-1). Adapted to salt water they increased their capacity, and the best duck secreted at a rate of 1215 mosmol·min-1 (1600 mosmol·kg-1). The best wild duck secreted at a rate of 1516 mosmol·min-1. Ducks in group 3 were used to examine the response to a hyperosmotic or an isoosmotic infusion. The amount of salt (NaCl) given per unit time was the same. Given a hyperosmotic solution their salt glands secreted at a high rate: 30 min after the infusion had stopped the ducks had excreted 94% of the sodium infused, 92.9% via the salt gland. Given an isoosmotic solution they secreted at a rate about half the infusion rate: 30 min after cessation of infusion they had excreted 73% of the sodium, 42.9% via the salt gland and the rest by the kidneys.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2019-07-13
    Description: A numerical lifting surface formulation, including computed results for planar wing cases is presented. This formulation, referred to as the vortex spline scheme, combines the adaptability to complex shapes offered by paneling schemes with the smoothness and accuracy of loading function methods. The formulation employes a continuous distribution of singularity strength over a set of panels on a paneled wing. The basic distributions are independent, and each satisfied all the continuity conditions required of the final solution. These distributions are overlapped both spanwise and chordwise. Boundary conditions are satisfied in a least square error sense over the surface using a finite summing technique to approximate the integral. The current formulation uses the elementary horseshoe vortex as the basic singularity and is therefore restricted to linearized potential flow. As part of the study, a non planar development was considered, but the numerical evaluation of the lifting surface concept was restricted to planar configurations. Also, a second order sideslip analysis based on an asymptotic expansion was investigated using the singularity spline formulation.
    Keywords: AERODYNAMICS
    Type: NASA-CR-2423 , D6-41093
    Format: application/pdf
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  • 3
    Publication Date: 2019-07-13
    Description: A new numerical formulation with computed results, is presented. This formulation combines the adaptability to complex shapes offered by paneling schemes with the smoothness and accuracy of the loading function methods. The formulation employs a continuous distribution of singularity strength over a set of panels on a paneled wing. The basic distributions are independent, and each satisfies all of the continuity conditions required of the final solution. These distributions are overlapped both spanwise and chordwise (termed 'spline'). Boundary conditions are satisfied in a least square error sense over the surface using a finite summing technique to approximate the integral.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 73-123 , Aerospace Sciences Meeting; Jan 10, 1973 - Jan 12, 1973; Washington, DC
    Format: text
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