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  • AERODYNAMICS  (1)
  • lipids  (1)
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  • 1
    ISSN: 1573-5176
    Keywords: fatty acids ; lipids ; Navicula sp. ; salinity
    Source: Springer Online Journal Archives 1860-2000
    Topics: Biology
    Notes: Abstract Navicula sp. (cf.N. tenelloides) was isolated from a salt marsh in Kuwait. The alga grew best with 0.5M NaCl, but abundant growth still occurred up to 2.5M NaCl. The total lipid content and the carotene to chlorophyll ratio of the cells increased with increasing salinity of the medium from 0.5 to 1.7M NaCl, but declined with 2.5M NaCl. Irrespective of the medium salinity, the major lipid class was that of triacylglycerols. The predominant fatty acids in the total lipids of cells grown at different NaCl concentrations were palmitic (16:0) and palmitoleic (16:1) acids; eicosapentaenoic acid (20:5) made up 8–9% of the total fatty acids. The fatty acid composition of the individual lipid classes of cells grown at different salinities is described. The highest concentration of 20:5 occurred in monogalactosyldiacylglycerols and digalactosyldiacylglycerols. In view of the rather small size of this diatom, its halotolerance and its fair content of 20:5, it is suggested as a potential food source for the mariculture industry.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2013-08-31
    Description: The application of stability theory in Laminar Flow Control (LFC) research requires that density and velocity profiles be specified throughout the viscous flow field of interest. These profile values must be as numerically accurate as possible and free of any numerically induced oscillations. Guidelines for the present research project are presented: develop an efficient and accurate procedure for solving the 3-D boundary layer equation for aerospace configurations; develop an interface program to couple selected 3-D inviscid programs that span the subsonic to hypersonic Mach number range; and document and release software to the LFC community. The interface program was found to be a dependable approach for developing a user friendly procedure for generating the boundary-layer grid and transforming an inviscid solution from a relatively coarse grid to a sufficiently fine boundary-layer grid. The boundary-layer program was shown to be fourth-order accurate in the direction normal to the wall boundary and second-order accurate in planes parallel to the boundary. The fourth-order accuracy allows accurate calculations with as few as one-fifth the number of grid points required for conventional second-order schemes.
    Keywords: AERODYNAMICS
    Type: Research in Natural Laminar Flow and Laminar-Flow Control, Part 2; p 517-545
    Format: application/pdf
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