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  • AERODYNAMICS  (2)
  • Cell & Developmental Biology  (1)
  • 2000-2004
  • 1975-1979  (3)
  • 1978  (3)
  • 1
    Electronic Resource
    Electronic Resource
    New York, NY [u.a.] : Wiley-Blackwell
    Journal of Cellular Physiology 95 (1978), S. 333-341 
    ISSN: 0021-9541
    Keywords: Life and Medical Sciences ; Cell & Developmental Biology
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology , Medicine
    Notes: The object of this study was to develop a map of G1 phase on the basis of the progressive changes taking place in the morphology of the prematurely condensed chromosomes as the cells traverse through G1 and then use this technique to determine the cell cycle location of normal and transformed cell populations in plateau phase. The morphology of the prematurely condensed chromosomes (PCC) of G1 cells in random populations was found to be highly variable. For a better understanding of the relationship between the morphology of the G1-PCC and their position within G1 phase, synchronized populations of Chinese hamster ovary (CHO) cells in early, mid-, and late G1 phase were fused with mitotic cells. Early G1 cells resulted in highly condensed G1-PCC, while late G1 cells gave very extended G1-PCC. Mid-G1 cells resulted in PCC of intermediate condensation. To test the validity of these criteria for mapping the position of a cell in the cell cycle, synchronous G1 cell populations were treated with a variety of metabolic inhibitors. Cycloheximide and actinomycin D were shown to block cell in early G1 phase, while excess thymidine and hydroxyurea blocked cells in early S phase. The results presented here indicate that, upon reaching plateau phase, normal cell populations (BALB-C mouse 3T3, human PA-2, and WI 38) stop in early G1, while most cells in transformed cell lines (CHO, HeLa, and mouse SV-3T3) accumulate in late G1.
    Additional Material: 8 Ill.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2019-06-27
    Description: A new device was proposed for alleviating high angle-of-attack side force on slender, pointed forebodies. A symmetrical pair of separation strips in the form of helical ridges are applied to the forebody to disrupt the primary lee-side vortices and thereby avoid the instability that produces vortex asymmetry. Preliminary wind tunnel tests at Mach 0.3 and Reynolds no. 5,250,000 on a variety of forebody configurations and on a wing-body combination at angles of attack up to 56 degrees, demonstrated the effectiveness of the device.
    Keywords: AERODYNAMICS
    Type: NASA-CR-145361
    Format: application/pdf
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  • 3
    Publication Date: 2019-06-27
    Description: The configuration consisted of a 30 deg -swept, untapered, untwisted wing utilizing a low-moment cambered airfoil of 20 percent streamwise thickness designed for low wave drag at M = 0.6, C sub L = 0.4. The tests covered a range of Mach numbers 0.3 to 0.725 and chord Reynolds number 1,100,000 to 2,040,000, angles of attack up to model buffet and sideslip angles + or - 4 deg. Configuration build up, wing pod filleting, airfoil modification and trailing edge control deflection effects were briefly investigated. Three wing tip vertical tail designs were also tested. Wing body filleting and a simple airfoil modification both produced increments to maximum lift/drag ratio. Addition of pods eliminated pitch instability of the basic wing. While the magnitude of these benefits probably was Reynolds number sensitive, they underline the potential for improving the aerodynamics of the present configuration. The cruise parameter (product of Mach number and lift/drag ratio) attained a maximum close to the airfoil design point. The configuration was found to be positively stable with normal control effectiveness about all three axes in the Mach number and C sub L range of interest.
    Keywords: AERODYNAMICS
    Type: NASA-TM-78767
    Format: application/pdf
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