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  • 1
    Electronic Resource
    Electronic Resource
    Chromosomal Localization of the ε1, ε3, and ζ1 Subunit Genes of the Human NMDA Receptor Channel
    Amsterdam : Elsevier
    Biochemical and Biophysical Research Communications 197 (1993), S. 922-926 
    Details
    ISSN: 0006-291X
    Source: Elsevier Journal Backfiles on ScienceDirect 1907 - 2002
    Topics: Biology , Chemistry and Pharmacology , Physics
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1006/bbrc.1993.2567
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  • 2
    Electronic Resource
    Electronic Resource
    Unstable expansion of CAG repeat in hereditary dentatorubral–pallidoluysian atrophy (DRPLA) (1994)
    [s.l.] : Nature Publishing Group
    Nature genetics 6 (1994), S. 9-13 
    Details
    ISSN: 1546-1718
    Source: Nature Archives 1869 - 2009
    Topics: Biology , Medicine
    Notes: [Auszug] Hereditary dentatorubral–pallidoluysian atrophy (DRPLA) is an autosomal dominant neurologic disorder characterized by variable combinations of myoclonus, epilepsy, cerebellar ataxia, choreoathetosis and dementia. By specifically searching published brain cDNA sequences for the presence of CAG ...
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1038/ng0194-9
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  • 3
    Electronic Resource
    Electronic Resource
    Unsteady interaction of shock wave diffracting around a circular cylinder in air (1991)
    Springer
    Acta mechanica Sinica 7 (1991), S. 295-299 
    Details
    ISSN: 1614-3116
    Keywords: shock wave diffraction ; large flow field around a cylinder ; pulsed laser holographic interferometry ; isopycnics ; complex interaction of curved shocks
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Notes: Abstract The reflection and diffraction of a planar shock wave around a circular cylinder are a typical problem of the complex nonlinear shock wave phenomena in literature. It has long been studied experimentally, analytically as well as numerically. Takayama in 1987 obtained clear experimental pictures of isopycnics in shock tube under the condition that the impinging shock wave propagates as far as 3 diameters away from the cylinder. To know more completely the whole unsteady process, it is desirable to get experimental results in a region which is more than 10 diameters away from the cylinder. This is what has been done in this paper by using the pulsed laser holographic interferometry for several shock Mach numbers of the impinging shock. Results for several moments are shown, giving more knowledge about the whole unsteady flow field. This is useful for a reliable and complete understanding of the changing force acting on the cylinder, and provides interesting data to check the performance of many recently developed high resolution numerical methods for unsteady shock wave calculation.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/BF02486736
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    Paper (German National Licenses)
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  • 4
    Electronic Resource
    Electronic Resource
    The gene for Machado–Joseph disease maps to human chromosome 14q (1993)
    [s.l.] : Nature Publishing Group
    Nature genetics 4 (1993), S. 300-304 
    Details
    ISSN: 1546-1718
    Source: Nature Archives 1869 - 2009
    Topics: Biology , Medicine
    Notes: [Auszug] Machado–Joseph disease (MJD) is an autosomal dominant, multisystem neurodegenerative disorder involving predominantly cerebellar, pyramidal, extrapyramidal, motor neuron and oculomotor systems. Although it was first reported in families of Portuguese–Azorean descent, MJD has also been ...
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1038/ng0793-300
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  • 5
    Electronic Resource
    Electronic Resource
    Three-dimensional shock wave reflection over a corner of two intersecting wedges (1997)
    Springer
    Shock waves 7 (1997), S. 107-121 
    Details
    ISSN: 1432-2153
    Keywords: Key words: 3-D Flow Visualization, Holographic Interferometry, Numerical Analysis, Shock Reflection
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics , Technology
    Notes: Abstract. This paper presents an experimental and numerical investigation of three-dimensional shock wave reflections over a corner of two wedges intersecting perpendicularly in a shock tube. Experiments were conducted in a $100\,{\rm mm} \times 180\,{\rm mm}$ diaphragmless shock tube equipped with double-exposure diffuse holographic interferometry in which the time interval between the first and second exposure was set to be $1 \,{\rm \mu s}$ . This arrangement clearly visualized complex configurations of three-dimensional shock wave reflections. A numerical study was also carried out for interpreting these holographic interferometric observations by using the Weighted Average Flux (WAF) method to solve the three-dimensional unsteady compressible Euler equations. It was found that along the line of the intersection of these two wedges, two Mach stems intersected each other resulting in the formation of a Mach stem which leaned forward.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/s001930050067
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  • 6
    Electronic Resource
    Electronic Resource
    Numerical and experimental study of a micro-blast wave generated by pulsed-laser beam focusing (1998)
    Springer
    Shock waves 8 (1998), S. 337-349 
    Details
    ISSN: 1432-2153
    Keywords: Key words:Micro-blast wave, Laser focusing, Numerical simulation, Flow visualization, Blast-wave reflection
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics , Technology
    Notes: Abstract. This paper describes a numerical and experimental study of a micro-blast wave which is produced from the source of several tens microns in dia. and propagates in the length scale of a few centimeter in diameter. The micro-blast wave was generated by focusing a Nd:Glass pulsed-laser beam in ambient air. Its propagation and reflection were visualized by using double exposure holographic interferometry and simulated numerically using the dispersion-controlled scheme to solve the Euler and Navier-Stokes equations with initial conditions of a point-source explosion specified with the Taylor similarity law. Good agreement was obtained between numerical solutions and experimental results, and this spherical micro-blast wave was shown to be a handy model of blast waves created in large scale explosions.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/s001930050126
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  • 7
    Electronic Resource
    Electronic Resource
    Evolution of shock waves and the primary vortex loop discharged from a square cross-sectional tube (1999)
    Springer
    Shock waves 9 (1999), S. 1-10 
    Details
    ISSN: 1432-2153
    Keywords: Key words:Numerical simulations, Holographic interferometry, Shock tube, Numerical flow visualization, Shock waves, Vortex loop
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics , Technology
    Notes: Abstract. In this paper, a numerical and experimental investigation of the evolution of a transmitting shock wave and its associated primary vortex loop, which are discharged from the open end of a square cross-sectional tube, is described. The experiments were conducted in the square tube connected to a diaphragmless shock tube and the flowfield was visualized from the axial direction with diffusive holographic interferometry. The numerical simulations were carried out by solving the three-dimensional Euler equations with a dispersion-controlled scheme. The numerical results were displayed in the form of interferograms to compare them with experimental interferograms. Good agreement between the numerical and experimental results was obtained. More detailed numerical calculations were carried out, from which the three-dimensional transition of the shock wave configuration from an initial planar to a spherical shape and the development of the primary vortex loop from a square shaped to a three-dimensional structure were clearly observed and interpreted.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/s001930050133
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  • 8
    Electronic Resource
    Electronic Resource
    Characteristics of an annular vertical diaphragmless shock tube (2000)
    Springer
    Shock waves 10 (2000), S. 151-158 
    Details
    ISSN: 1432-2153
    Keywords: Key words: Vertical co-axial diaphragmless shock tube, Rubber diaphragm, Repeatability of shock tube, Toroidal shock wave focusing
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics , Technology
    Notes: Abstract. This paper reports on the characteristics of a compact vertical diaphragmless shock tube, which was constructed and tested in the Shock Wave Research Center to study experimentally the behavior of toroidal shock waves. It is 1.15 m in height and has a self-sustained co-axial vertical structure consisting of a 100 mm i.d. outer tube and an 80 mm o.d. inner tube. To create a ring shaped shock wave between the inner and outer tubes, a rubber sheet is inserted to separate a high pressure driver gas from a test gas, which is bulged with auxiliary high pressure helium from the behind. When the rubber membrane is contracted by the sudden release of the auxiliary gas so as to break the seal, shock waves are formed. Special design features of the shock tube are described and their role in producing repeatable shock waves is discussed. Its special opening characteristics make possible the production of annular shaped shock waves that are unlikely met with a conventional tube that uses rupturing diaphragms. Performance of the shock tube is evaluated in terms of the shock wave Mach numbers and the measured flow properties. It eventually showed a higher degree of repeatability and the scatter in the shock wave Mach numbers Ms was found to be 0.2% for Ms ranging from 1.1 to 1.8. The shock wave Mach number so far measured agreed very well with the simple shock tube theory.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/s001930050001
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  • 9
    Electronic Resource
    Electronic Resource
    Experimental investigation on tunnel sonic boom (1995)
    Springer
    Shock waves 5 (1995), S. 127-138 
    Details
    ISSN: 1432-2153
    Keywords: Impulsive pressure wave ; Piston problem ; Perforated wall ; Railway tunnel ; Shock wave generation ; Sonic boom
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics , Technology
    Notes: Abstract Upon the entrance of a high-speed train into a relatively long train tunnel, compression waves are generated in front of the train. These compression waves subsequently coalesce into a weak shock wave so that a unpleasant sonic boom is emitted from the tunnel exit. In order to investigate the generation of the weak shock wave in train tunnels and the emission of the resulting sonic boom from the train tunnel exit and to search for methods for the reduction of these sonic booms, a 1∶300 scaled train tunnel simulator was constructed and simulation experiments were carried out using this facility. In the train tunnel simulator, an 18 mm dia. and 200 mm long plastic piston moves along a 40 mm dia. and 25 m long test section with speed ranging from 60 to 100 m/s. The tunnel simulator was tilted 8° to the floor so that the attenuation of the piston speed was not more than 10 % of its entrance speed. Pressure measurements along the tunnel simulator and holographic interferometric optical flow visualization of weak shock waves in the tunnel simulator clearly showed that compression waves, with propagation, coalesced into a weak shock wave. Although, for reduction of the sonic boom in prototype train tunnels, the installation of a hood at the entrance of the tunnels was known to be useful for their suppression, this effect was confirmed in the present experiment and found to be effective particularly for low piston speeds. The installation of a partially perforated wall at the exit of the tunnel simulator was found to smear pressure gradients at the shock. This effect is significant for higher piston speeds. Throughout the series of train tunnel simulator experiments, the combination of both the entrance hood and the perforated wall significantly reduces shock overpressures for piston speeds ofu p ranging from 60 to 100 m/s. These experimental findings were then applied to a real train tunnel and good agreement was obtained between the tunnel simulator result and the real tunnel measurements.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/BF01435520
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