Institution
Japan Aerospace Exploration Agency
Facility•Tokyo, Japan•
About: Japan Aerospace Exploration Agency is a facility organization based out in Tokyo, Japan. It is known for research contribution in the topics: Galaxy & Telescope. The organization has 4327 authors who have published 12054 publications receiving 208330 citations.
Papers published on a yearly basis
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Goddard Space Flight Center1, Netherlands Institute for Space Research2, University of Genoa3, Lawrence Livermore National Laboratory4, University of Maryland, Baltimore County5, Kanazawa University6, Rikkyo University7, Tokyo Metropolitan University8, University of Wisconsin-Madison9, Nagoya University10, Tohoku Gakuin University11, Kindai University12, Tohoku University13, Japan Aerospace Exploration Agency14, Nara Women's University15, Universities Space Research Association16, Tokyo University of Science17, Aoyama Gakuin University18, Yale University19, Saitama University20, Tokyo Institute of Technology21
TL;DR: The Astro-H (Hitomi) Soft X-Ray Spectrometer (SXS) was designed to achieve an energy resolution better than 7 eV over the 0.3-12 keV energy range and operate for more than 3 years in orbit as discussed by the authors.
Abstract: We present the overall design and performance of the Astro-H (Hitomi) Soft X-Ray Spectrometer (SXS). The instrument uses a 36-pixel array of x-ray microcalorimeters at the focus of a grazing-incidence x-ray mirror Soft X-Ray Telescope (SXT) for high-resolution spectroscopy of celestial x-ray sources. The instrument was designed to achieve an energy resolution better than 7 eV over the 0.3-12 keV energy range and operate for more than 3 years in orbit. The actual energy resolution of the instrument is 4-5 eV as demonstrated during extensive ground testing prior to launch and in orbit. The measured mass flow rate of the liquid helium cryogen and initial fill level at launch predict a lifetime of more than 4 years assuming steady mechanical cooler performance. Cryogen-free operation was successfully demonstrated prior to launch. The successful operation of the SXS in orbit, including the first observations of the velocity structure of the Perseus cluster of galaxies, demonstrates the viability and power of this technology as a tool for astrophysics.
108 citations
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TL;DR: In this paper, a uniform analysis of the ROSAT HRI and the ASCA GIS/SIS data for 79 distant clusters of galaxies in the redshift range 0.1 < z < 0.82 is presented.
Abstract: We present a uniform analysis of the ROSAT HRI and the ASCA GIS/SIS data for 79 distant clusters of galaxies in the redshift range 0.1 < z < 0.82 to study the global structures of the intracluster medium. We have constructed an X-ray catalog consisting of the largest sample of clusters in the redshift range for which pointed X-ray observations were carried out with both the observatories. We determined the emission-weighted X-ray temperatures of the clusters with ASCA, while we studied surface brightness distribution with the ROSAT HRI utilizing the isothermal β model. We investigated the statistical properties and trends for redshift evolution of the X-ray parameters including the temperature, the density profile of the intracluster gas and the gas-mass fraction within r500. We also present correlations of the cluster parameters with the X-ray temperature and with the core radius and compare them with the predictions of the self-similar model, from which we discuss the possible origin of the double structure discovered in the core radius distribution.
108 citations
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TL;DR: In this paper, a survey of numerical experiments from 12 different flux functions in one-and two-dimensional contexts is presented, and it is found that there are at least two kinds of shock instabilities: one is one-dimensional and the other is multidimensional.
Abstract: Shock-capturing finitevolumeschemesoftengiverisetoanomalousresultsinhypersonic flow.Wepresentawideranging survey of numerical experiments from 12 different flux functions in one- and two-dimensional contexts. Included is a recently developed function that satisfies the second law of thermodynamics. It is found here that there are at least two kinds of shock instabilities: one is one-dimensional and the other is multidimensional. According to the results, the former does not appear if a flux function satisfies the second law of thermodynamics, and the latter is suppressed by an additional dissipation with a multidimensional character. However, such dissipation has no effect on the one-dimensional mode. Among the flux functions investigated, no universally stable schemes are found that arefreefrombothone-andmultidimensionalshockinstabilities.Theappearanceoftheseinstabilitiesdependsonthe relative positioning of the shock on the grid.
108 citations
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TL;DR: In this paper, the authors used the recently acquired data to better characterize the contribution of continental sources to the aerosol, ozone, and related trace species concentrations over the North Pacific.
Abstract: [1] In the winter and spring of 2002, airborne and ground-based measurements of O3, aerosols, and their precursors were made in the eastern and western North Pacific regions. Three field studies were conducted by an international team of scientists collaborating as part of the Intercontinental Transport and Chemical Transformation (ITCT) program, an activity of the International Global Atmospheric Chemistry (IGAC) project of the International Geosphere-Biosphere Program (IGBP). Previous measurements have indicated that the transport of Asian emissions across the North Pacific Ocean influences the concentrations of trace tropospheric species over the Pacific and even the west coast of North America. In this special section, the recently acquired data are used to better characterize the contribution of continental sources to the aerosol, ozone, and related trace species concentrations over the North Pacific. This overview is aimed at providing the operational and logistical context of the study and introducing the principal findings and conclusions that have been drawn from the results.
107 citations
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TL;DR: In this paper, the effect of grid resolution and grid quality on aerodynamic drag prediction has been examined in detail and recommendations for improvements in mesh generation technology which have the potential to impact the state-of-the-art of aerodynamic prediction are given.
Abstract: The drag prediction workshop series (DPW), held over the last six years, and sponsored by the AIAA Applied Aerodynamics Committee, has been extremely useful in providing an assessment of the state-of-the-art in computationally based aerodynamic drag prediction. An emerging consensus from the three workshop series has been the identification of spatial discretization errors as a dominant error source in absolute as well as incremental drag prediction. This paper provides an overview of the collective experience from the worksho
series regarding the effect of grid-related issues on overall drag prediction accuracy. Examples based on workshop results are used to illustrate the effect of grid resolution and grid quality on drag prediction, and grid convergence behavior is examined in detail. For fully attached flows, various accurate and successful workshop results are demonstrated, while anomalous behavior is identified for a number of cases involving substantial regions of separated
flow. Based on collective workshop experiences, recommendations for improvements in mesh generation technology which have the potential to impact the state-of-the-art of aerodynamic drag prediction are given.
106 citations
Authors
Showing all 4340 results
Name | H-index | Papers | Citations |
---|---|---|---|
Yasushi Fukazawa | 135 | 882 | 64424 |
Jun Kataoka | 121 | 603 | 54274 |
Tadayuki Takahashi | 112 | 932 | 57501 |
Takaaki Tanaka | 105 | 321 | 41804 |
Yasunobu Uchiyama | 105 | 373 | 39610 |
Satoshi Tanaka | 96 | 739 | 76264 |
Masashi Hazumi | 87 | 708 | 29603 |
K. Izumi | 84 | 229 | 53205 |
Carolus J. Schrijver | 81 | 297 | 29858 |
Satoru Takahashi | 79 | 589 | 28007 |
Chris Done | 79 | 457 | 23210 |
Yasuo Doi | 79 | 370 | 33445 |
Poshak Gandhi | 75 | 481 | 18419 |
Alan M. Title | 74 | 203 | 21923 |
Yoshihiro Ueda | 72 | 576 | 25787 |