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  • Muller  (3)
  • BTI  (1)
  • Crustal deformation (cf. Earthquake precursor: deformation or strain)  (1)
  • Fluid Mechanics and Thermodynamics  (1)
  • 34.50.Fa
  • 2000-2004  (4)
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  • 1
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    In:  Eos, Trans., Am. Geophys. Un., Warszawa, American Geophysical Union, vol. 81, no. 13, pp. 137 & 140, pp. L08304, (ISSN: 1340-4202)
    Publication Date: 2000
    Keywords: Stress ; Proceedings of a conference ; Stress measurements ; Borehole breakouts ; BTI ; cracks and fractures (.NE. fracturing) ; Geodesy ; Global Positioning System ; Very Long Baseline Interferometry ; Strain ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Applied geophysics ; Muller ; World Stress Map (Project) ; Euroconferences
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  • 2
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    In:  Tectonophysics, Kunming, China, 3-4, vol. 361, no. 1-2, pp. 21-35, pp. 2276, (ISSN: 1340-4202)
    Publication Date: 2003
    Keywords: Stress ; Borehole geophys. ; Borehole breakouts ; Mueller ; Muller
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  • 3
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    In:  Eos, Trans., Am. Geophys. Un., Oxford and Edinburgh, Blackwell Scientific Publications, vol. 85, no. 49, pp. 521 & 529, pp. 1484, (ISBN: 0534351875, 2nd edition)
    Publication Date: 2004
    Keywords: Stress ; software ; Plate tectonics ; Tectonics ; Earthquake hazard ; data ; base ; Fault plane solution, focal mechanism ; Borehole breakouts ; quality ; World Stress Map (Project) ; Muller ; Mueller
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  • 4
    Publication Date: 2019-07-13
    Description: A method of minimizing numerical errors, and improving nonlinear stability and accuracy associated with low Mach number computational aeroacoustics (CAA) is proposed. The method consists of two levels. From the governing equation level, we condition the Euler equations in two steps. The first step is to split the inviscid flux derivatives into a conservative and a non-conservative portion that satisfies a so called generalized energy estimate. This involves the symmetrization of the Euler equations via a transformation of variables that are functions of the physical entropy. Owing to the large disparity of acoustic and stagnation quantities in low Mach number aeroacoustics, the second step is to reformulate the split Euler equations in perturbation form with the new unknowns as the small changes of the conservative variables with respect to their large stagnation values. From the numerical scheme level, a stable sixth-order central interior scheme with a third-order boundary schemes that satisfies the discrete analogue of the integration-by-parts procedure used in the continuous energy estimate (summation-by-parts property) is employed.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: 5th International Conference on Spectral and High Order Methods; Jun 11, 2001 - Jun 15, 2001; Uppsala; Sweden
    Format: application/pdf
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