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| 1 | Study on Shock Wave and Turbulent Boundary Layer Interactions in a Square Duct at Mach 2 and 4显示文摘在这份报纸,为在管的超声的内部流动的调查的马赫 4 超声的风隧道的轮廓第一被描述。第二, 2 和马赫 4 伪吃惊在方形的管挥动的马赫的地点,结构和特征被颜色 schlieren 相片和管墙压力调查变化大小。最后,墙砍有马赫 4 伪吃惊的方形的管的墙挥动的方面,顶和底部上的压力分布是由 shear 的调查品质上压力敏感的液体水晶可视化方法。在第一震动下面的方面墙边界层分离区域在最高的墙附近是狭窄的,当在第一震动下面的方面墙边界层分离区域在底部墙附近是很宽的时。关键词超声的内部流动 - 伪吃惊波浪 - 流动可视化 - 砍压力敏感的液体水晶 CLC 数字 O357. | Hiromu SUGIYAMA Ryojiro MINATO Kazuhide MIZOBATA Akira TOJO Yohei MUTO | 2006 | Journal of Thermal Science2006，15，1： | 3 |
| 2 | Role of p38 MAP kinase pathway in a toxin-induced model of hemolytic uremic syndrome显示文摘 | Xue Jun Fu Kazumoto Iijima Kandai Nozu Kiyoshi Hamahira Ryojiro Tanaka Tatsuya Oda Norishige Yoshikawa Masafumi Matsuo | 2004 | Pediatric Nephrology2004，，8： | 1 |
| 3 | Pathophysiology and treatment of IgA nephropathy in children显示文摘 | N. Yoshikawa Ryojiro Tanaka Kazumoto Iijima | 2001 | Pediatric Nephrology2001，，5： | 1 |
| 4 | Pathophysiology and treatment of IgA nephropathy in children显示文摘 | Norishige Y Ryojiro T Kazumoto I | 2001 | Pediatr Nephrol2001，16，： | 1 |
| 5 | OCRL1 mutations in patients with Dent disease phenotype in Japan显示文摘 | Takashi Sekine Kandai Nozu Rashmi Iyengar Xue Jun Fu Masafumi Matsuo Ryojiro Tanaka Kazumoto Iijima Emiko Matsui Yutaka Harita Jun Inatomi Takashi Igarashi | 2007 | Pediatric Nephrology2007，，7： | 1 |
| 6 | OCRL1 mutations in patients with Dent disease phenotype in Japan显示文摘 | Takashi Sekine Kandai Nozu Rashmi Iyengar Xue Jun Fu Masafumi Matsuo Ryojiro Tanaka Kazumoto Iijima Emiko Matsui Yutaka Harita Jun Inatomi Takashi Igarashi | 2007 | Pediatric Nephrology2007，，7： | 1 |
| 7 | Overspeeding characteristics of turbomachinery for gas generator cycle air turbo ramjet engine显示文摘The main interest in the current study focuses on the possibility of overspeeding for the gas-generator cycle air turbo ramjet(GG-ATR)engine.The authors developed the air turbo ramjet engine and investigated its compressor performance.Based on those data,the authors developed the analytical code for the air turbo ramjet engine,which calculates the performances of turbomachinery,gas-generator,and ram combustor.The previous study described that the rotor overspeeding would not occur in the air turbo rocket engine.However,the current results show that degraded ram combustion can decrease the compressor pressure ratio and the compressor power.This reduced compressor power can cause overspeeding for the air turbo ramjet engine.The experimental results of compressor power and turbine inlet pressure support those analytical results. | Ryojiro Minato Daisuke Nakata Masaharu Uchiumi Ryoji Imai Kazuyuki Higashino | 2022 | Propulsion and Power Research2022，11，4： | 0 |
| 8 | Low toxic nitromethane based monopropellant for gas generator cycle air turbo ramjet engine显示文摘The present study proposes ethanol-nitromethane mixture as a safe, storable, andlow toxic monopropellant for a gas generator cycle air turbo ramjet engine and evaluates itspropulsion performance. The present study proposes that nitromethane is mixed with ethanolto adjust gas generator combustion temperature. The author developed the computational codefor the present analysis and verified its accuracy. The specific thrust of ethanol-nitromethane isnearly identical to that of ethanol-liquified oxygen and is higher than methanol-hydroxylammonium nitrate aqueous solution and hydrazine. Hydrazine has the highest Ispamong the propellants in the present analysis. However, Isp of ethanol-nitromethane is nearlyequal to that of ethanol-liquified oxygen and higher than those of methanol-hydroxylammonium nitrate aqueous solution, and hydroxyl terminated polybutadiene-ammonium perchlorate. With the propellant-to-air ratio range in the present study, ethanol-nitromethane has the stoichiometric condition at the ram combustor around the propellant-to-air ratio range from 0.2 to 0.25 and can obtain high ram combustion temperature. This resultis favorable for ethanol-nitromethane because it improves the specific thrust and the specificimpulse. Therefore, ethanol-nitromethane can be a promising low-toxic liquid monopropellantfor the air turbo ramjet engine. | Ryojiro Minato | 2022 | Propulsion and Power Research2022，11，3： | 0 |
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