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  • AERODYNAMICS  (2)
  • cerebrospinal fluid  (1)
  • 1995-1999
  • 1985-1989  (3)
  • 1985  (3)
Collection
Publisher
Years
  • 1995-1999
  • 1985-1989  (3)
Year
  • 1
    Electronic Resource
    Electronic Resource
    Springer
    European journal of clinical pharmacology 29 (1985), S. 225-229 
    ISSN: 1432-1041
    Keywords: moxalactam ; antibiotic ; plasma level ; cerebrospinal fluid ; high performance liquid chromatography ; assay method
    Source: Springer Online Journal Archives 1860-2000
    Topics: Chemistry and Pharmacology , Medicine
    Notes: Summary A sensitive and reproducible method for the measurement of moxalactam in plasma and cerebrospinal fluid is described. Plasma proteins were removed by precipitation with ice-cold methanol at pH 5.6 and centrifugation. The supernatant was analysed by HPLC on a µ-Bondapack/phenyl column, with a mobile phase of acetonitrile/water/PIC Reagent A (20/80/1), and detection at 280 nm. The calibration curve was linear for plasma concentrations from 10 µg/ml to 60 µg/ml. Reproducibility was 4.7% (coefficient of variation) for within-day analysis and 13.8% for day-to-day analysis. Plasma concentrations in 9 moxalactam-treated patients with severe infections ranged from 0.9 µg/ml to 409 µg/ml. Individual pharmacokinetic parameters were calculated using a personal computer. In selected cases moxalactam concentrations were also determined in cerebrospinal fluid and tracheal aspirates.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2011-08-19
    Keywords: AERODYNAMICS
    Type: Journal of Spacecraft and Rockets (ISSN 0022-4650); 22; 304-308
    Format: text
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  • 3
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    In:  Other Sources
    Publication Date: 2019-06-28
    Description: This paper presents a review of circulation control technology, its history, status and areas for further research and development. A brief description of the basic performance characteristics of circulation control airfoils are presented together with a more detailed discussion of some of the more important aerodynamic parameters dependencies. The unique capability of the airfoils to develop high lift coefficients independent of incidence over a range of operating conditions is demonstrated. Consideration is also given to the various stall conditions that have been experimentally observed and to the various theoretical formulations that have been attempted to explain these phenomena.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 85-0204
    Format: text
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