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  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Journal of bioenergetics and biomembranes 21 (1989), S. 573-588 
    ISSN: 1573-6881
    Keywords: Gastric H+ transport ; ATPase ; omeprazole ; K+ site
    Source: Springer Online Journal Archives 1860-2000
    Topics: Biology , Chemistry and Pharmacology , Physics
    Notes: Abstract The gastric H+ + K+ ATPase is a member of the phosphorylating class of transport ATPase. Based on sequence homologies and CHO content, there may be ab subunit associated with the catalytic subunit of the H+ + K+ ATPase. Its function, if present, is unknown. The pump catalyzes a stoichiometric exchange of H+ for K+, but is also able to transport Na+ in the forward direction. This suggests that the transport step involves hydronium rather than protons. The initial binding site is likely to contain a histidine residue to account for the high affinity of the cellular site. The extracellular site probably lacks this histidine, so that a low affinity for hydronium allows release into a solution of pH 0.8. Labelling with positively charge, luminally reactive reagents that block ATPase and pump activity has shown that a region containing H5 and H6 and the intervening luminal loop is involved in necessary conformational changes for normal pump activity. The calculated structure of this loop shows the presence of ana helical,b turn, andb strand sector, with negative charges close to the membrane domain. This sector provides a possible site of interaction of drugs with the H+ + K+ ATPase, and may be part of the K+ pathway in the enzyme.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2019-06-28
    Description: An inverse design procedure was developed for the design of a mistuned rotor. The design requirements are that the stability margin of the eigenvalues of the aeroelastic system be greater than or equal to some minimum stability margin, and that the mass added to each blade be positive. The objective was to achieve these requirements with a minimal amount of mistuning. Hence, the problem was posed as a constrained optimization problem. The constrained minimization problem was solved by the technique of mathematical programming via augmented Lagrangians. The unconstrained minimization phase of this technique was solved by the variable metric method. The bladed disk was modelled as being composed of a rigid disk mounted on a rigid shaft. Each of the blades were modelled with a single tosional degree of freedom.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-CR-173179 , NAS 1.26:173179 , GTL-176
    Format: application/pdf
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  • 3
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-06-28
    Description: In the present inverse design procedure for the optimum mistuning of a high bypass ratio shroudless fan that is modeled as a cascade of blades (each with a single torsional degree-of-freedom), linearized supersonic aerodynamic theory is used to compute the unsteady aerodynamic forces in the 'influence coefficient' form at a typical blade section. The mistuning pattern is then numerically optimized in order to achieve a specified increase in the aeroelastic stability margin with a minimum amount of mistuning. If the blades are self-damped, an optimized mistuning pattern can be found that achieves a given stability margin for a much lower level of mistuning than required for the alternate mistuning pattern, which requires only two blade frequencies and is relatively insensitive to implementation errors.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: ASME PAPER 84-GT-196
    Format: text
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