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  • 1
    facet.materialart.
    Unbekannt
    In:  Eos, Trans., Am. Geophys. Un., Reykjavík, Icelandic Meteorological Office, Ministry for the Environment, University of Iceland, vol. 77, no. 48, pp. 477, 480-482, pp. L05306, (ISSN: 1340-4202)
    Publikationsdatum: 1996
    Schlagwort(e): Seismic arrays ; PASScalingIReservoir induced seismicity ; seismic MomentA ; SEED ; ConvolutionE ; earth Core ; earth mantle ; boundary ; Subduction zone ; Anisotropy
    Standort Signatur Erwartet Verfügbarkeit
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  • 2
    facet.materialart.
    Unbekannt
    In:  J. Geophys. Res., Tokyo, Terra Scientific Publishing Company, vol. 96, no. 35, pp. 14429-14444, pp. L16602, (ISBN: 0534351875, 2nd edition)
    Publikationsdatum: 1991
    Schlagwort(e): Seismology ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Source parameters ; Subduction zone ; JGR
    Standort Signatur Erwartet Verfügbarkeit
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  • 3
    facet.materialart.
    Unbekannt
    In:  Nature, Tokyo, Terra Scientific Publishing Company, vol. 415, no. 6873, pp. 745-748, pp. L16602, (ISBN: 0534351875, 2nd edition)
    Publikationsdatum: 2002
    Beschreibung: Conditions in Earth's mantle can be inferred from seismic-wave velocities which reveal areas of anisotropy. Evidence emerges of such an area at mid-mantle level, associated with a subducting tectonic plate.
    Schlagwort(e): Anisotropy ; Seismology ; earth mantle ; Physical properties of rocks ; Subduction zone ; Plate tectonics
    Standort Signatur Erwartet Verfügbarkeit
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  • 4
    Publikationsdatum: 2003
    Schlagwort(e): CC 4 ; Coordinating Committee ; Continental Drilling ; ICDP
    Standort Signatur Erwartet Verfügbarkeit
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  • 5
    Publikationsdatum: 2006-10-26
    Beschreibung: Supersonic transport time and fuel problems - relation to air traffic control system
    Schlagwort(e): NAVIGATION
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 6
    facet.materialart.
    Unbekannt
    In:  Other Sources
    Publikationsdatum: 2011-08-16
    Beschreibung: Slender cone boundary layer transition under angle of attack at Mach 21 with promoted leeward and fixed windward ray
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: ; YAL SOCIETY (
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 7
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    Unbekannt
    In:  Other Sources
    Publikationsdatum: 2011-08-18
    Beschreibung: Laminar flow control is a technology with great potential for aircraft drag reduction. Stabilization of laminar boundary layers became known as natural laminar flow (NLF) and research led to the development of NLF airfoils. Research was also conducted on stabilization by suction, referred to as laminar flow control (LFC). Experiments demonstrated that extensive laminar flow could be achieved in flight. However, there remained doubts regarding the practicality of producing, with the technology then available, wing surfaces sufficiently smooth and wavefree to meet laminar-flow criteria and maintaining the wing surface quality in normal service. In 1976, the Aircraft Energy Efficiency (ACEE) program was begun by NASA to develop fuel-conservative technology for commercial transports. The progress of the ACEE program is discussed. Attention is given to LFC wing structures, and LFC leading-edge systems.
    Schlagwort(e): AERODYNAMICS
    Materialart: Aerospace America (ISSN 0740-722X); 22; 72-76
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 8
    facet.materialart.
    Unbekannt
    In:  Other Sources
    Publikationsdatum: 2011-08-16
    Beschreibung: Ablation effects on transition Reynolds number of hypersonic boundary layer on slender cones
    Schlagwort(e): FLUID MECHANICS
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 9
    facet.materialart.
    Unbekannt
    In:  Other Sources
    Publikationsdatum: 2011-08-16
    Beschreibung: The presented paper shows the effect of local Mach number on the turbulent disturbance spreading angle relative to the wall and on lateral disturbance spreading angles. Almost all the disturbances angles relative to the wall were determined from investigations where hot-wire contours or hot-film surveys of a 'laminar' boundary layer were obtained. Lateral disturbance spreading angles were obtained from investigations of various conditions including turbulent bursts, reported observations of transverse contamination, and observed transitional flow. It is noted that the disturbance spreading angle relative to the wall seems to remain essentially invariant with Mach number, while the lateral spreading angle decreases sharply with increasing Mach number up to about 6. The good agreement between lateral disturbance spreading angle data and data for the variation of turbulent jet spreading angle with Mach number implies that in the lateral dimension, turbulence in a boundary layer may develop essentially free of wall constraints (similar to a free shear layer).
    Schlagwort(e): FLUID MECHANICS
    Materialart: AIAA Journal; 10; July 197
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 10
    facet.materialart.
    Unbekannt
    In:  Other Sources
    Publikationsdatum: 2011-08-16
    Beschreibung: Experimental results suggest that the boundary-layer mean profiles in hypersonic flows may be highly transitional in the outer part of the boundary layer before the transition process is detected at the surface. Means of determining the initial location where the transition process begins in the outer part of the boundary layer are considered.
    Schlagwort(e): AERODYNAMICS
    Materialart: AIAA Journal; 10; May 1972
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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