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Research and Development Report (RR)
ISSN 2433-2216(Online)
ISSN 1349-1113( Print )

Results 161-180 of 349.

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161. 大気球研究報告 Research reports on high altitude balloons
(著者名) 宇宙航空研究開発機構
(Author) Japan Aerospace Exploration Agency
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-009 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(言語) jpn(資料番号) AA0063732000
162. 一般化最小残差(GMRES)法の安定性検証 The stability experiment of the Generalized Minimal Residual (GMRES) method
(著者名) 坂下 雅秀; 松尾 裕一; 村山 光宏
(Author) Sakashita, Masahide; Matsuo, Yuichi; Murayama, Mitsuhiro
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-008 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) In order to apply the GMRES (Generalized Minimal RESidual) method, faster and more stable than the L...
(言語) jpn(資料番号) AA0063731000
163. Effect of airframe configuration on condition of airflow to engine in hypersonic flow 極超音速気流中において機体形状がエンジンに流入する気流に及ぼす影響について
(著者名) 苅田 丈士; 加藤 周徳; 小寺 正敏; ほか
(Author) Kanda, Takeshi; Kato, Kanenori; Kodera, Masatoshi; et al.
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-007E (ISSN) 1349-1113
(刊行年月日) 2007-12-28
(抄録) The effect of the airframe configuration on the condition of the airflow to an engine was investigat...
(言語) eng(資料番号) AA0063730000
164. 将来宇宙輸送システムの概念設計ツールの開発について Development of optimal design and evaluation program for future space transportation system concept
(著者名) 鈴木 広一; 苅田 丈士; 甲斐 高志; ほか
(Author) Suzuki, Hirokazu; Kanda, Takeshi; Kai, Takashi; et al.
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-006 (ISSN) 1349-1113
(刊行年月日) 2008-01-31
(抄録) The Japan Space Exploration Agency (JAXA) is developing a concept design tool called SEAT (Systems E...
(言語) jpn(資料番号) AA0063606000
165. モンテカルロ法によるシステムの統計的評価 Stochastic system evaluation by Monte Carlo approach
(著者名) 元田 敏和
(Author) Motoda, Toshikazu
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-005 (ISSN) 1349-1113
(刊行年月日) 2007-12-28
(抄録) In the development of aerospace vehicles, pre-flight evaluation is essential because it is often une...
(言語) jpn(資料番号) AA0063729000
166. 飛行制御システムに用いる光励起固体リングレーザージャイロの基礎研究 Fundamental study of an optical pumping solid ring laser gyro for flight control system
(著者名) 滝沢 実
(Author) Takizawa, Minoru
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-004 (ISSN) 1349-1113
(刊行年月日) 2007-12-28
(抄録) Fundamental study of an Optical pumping solid Ring Laser Gyro (ORLG) for flight control system of an...
(言語) jpn(資料番号) AA0063728000
167. 熱力学的効果が同期旋回キャビテーションに与える影響 Influence of thermodynamic effect on synchronous rotating cavitation
(著者名) 吉田 義樹; 笹尾 好史; 沖田 耕一; ほか
(Author) Yoshida, Yoshiki; Sasao, Yoshifumi; Okita, Koichi; et al.
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-003 (ISSN) 1349-1113
(刊行年月日) 2007-09-28
(抄録) Synchronous rotating cavitation is one type of cavitation instability, causing synchronous shaft vib...
(言語) jpn(資料番号) AA0063533000
168. Straight line systemsの摂動系に対する衝撃波干渉条件について On shock interaction conditions for a perturbation of straight line systems
(著者名) 岸 恭子; 岩宮 敏幸; 高橋 匡康
(Author) Kishi, Kyoko; Iwamiya, Toshiyuki; Takahashi, Tadayasu
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-002 (ISSN) 1349-1113
(刊行年月日) 2007-10-31
(抄録) The purpose of this report is to prove the existence of 2 x 2 hyperbolic non-linear systems of conse...
(言語) jpn(資料番号) AA0063527000
169. Direct simulation Monte Carlo study of rotational relaxation of nitrogen using classical trajectory calculations and modified statistical inelastic cross-section model Direct simulation Monte Carlo study of rotational relaxation of nitrogen using classical trajectory calculations and modified statistical inelastic cross-section model
(著者名) 古浦 勝久; 中村 絹代; 溝渕 泰寛
(Author) Koura, Katsuhisa; Nakamura, Kinuyo; Mizobuchi, Yasuhiro
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-001E (ISSN) 1349-1113
(刊行年月日) 2007-07-31
(抄録) Direct Simulation Monte Carlo (DSMC) calculations of the rotational relaxation of nitrogen in an iso...
(言語) eng(資料番号) AA0063502000
170. 連続モデルに由来しない離散モデルの性質について An example of inconsistency between continuous and discrete models
(著者名) 相曽 秀昭; Abouziarov, Moustafa
(Author) Aiso, Hideaki; Abouziarov, Moustafa
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-050 (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) In numerical simulation two kinds of mathematical models are usually used, continuous models and dis...
(言語) jpn(資料番号) AA0063878000
171. 小型超音速実験機(ロケット実験機; NEXST-1)第2回飛行実験 The second flight experiment of the supersonic experimental airplane (NEXST-1)
(著者名) 大貫 武; 町田 茂; 吉田 憲司; ほか
(Author) Onuki, Takeshi; Machida, Shigeru; Yoshida, Kenji; et al.
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-049 (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) The flight trial of the unmanned experimental airplane was conducted by Japan Aerospace Exploration ...
(言語) jpn(資料番号) AA0063991000
172. CFD解析による航空機用燃焼器の空気孔配置の最適化 Optimization of air hole arrangement in aeroengine combustor by CFD analysis
(著者名) 飯野 淳; 牧田 光正; 野崎 理
(Author) Iino, Jun; Makida, Mitsumasa; Nozaki, Osamu
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-048 (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) The Japan Aerospace Exploration Agency (JAXA) has started TechCLEAN, 'Technology development project...
(言語) jpn(資料番号) AA0063940000
173. 軌道上組立用画像計測システム An image measurement system for on-orbit structure assembly by space robot
(著者名) 上村 平八郎; 西田 信一郎
(Author) Kamimura, Heihachiro; Nishida, Shinichiro
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-047 (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) A structure assembly is effective robot work, in order to build a large-sized structure on orbit and...
(言語) jpn(資料番号) AA0063990000
174. 超音速風洞におけるAGARD-B標準模型3分力試験 Force measurement tests of AGARD Calibration Model-B of supersonic wind tunnel
(著者名) 飯島 秀俊; 渡辺 光則; 神田 宏; ほか
(Author) Iijima, Hidetoshi; Watanabe, Mitsunori; Kanda, Hiroshi; et al.
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-046 (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) A series of wind tunnel tests had been conducted on AGARD (Advisory Group for Aerospace Research and...
(言語) jpn(資料番号) AA0063877000
175. 透過型校正器具を用いたワイドベースラインステレオの研究 Wide baseline stereo with a transparent calibration tool
(著者名) 片山 保宏
(Author) Katayama, Yasuhiro
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-045 (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) Estimating camera parameters is an important topic in the area of stereo vision. We proposed a new t...
(言語) jpn(資料番号) AA0063797000
176. 小型超音速実験機(NEXST-1)通信系統設計の飛行実験検証 Flight test verification of the radio communication systems design for non-powered supersonic experimental airplane NEXST-1
(著者名) 村上 義隆; 多田 章; 滝沢 実; ほか
(Author) Murakami, Yoshitaka; Tada, Akira; Takizawa, Minoru; et al.
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-044 (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) The second flight trial of NEXST-1 (National EXperimental Supersonic Transport-1) non-powered and un...
(言語) eng(資料番号) AA0063919000
177. パイロット偏心型低NO(x)燃料ノズルの開発 Development of low-NO(x) fuel nozzle with eccentric pilot fuel injector
(著者名) 山本 武; 黒澤 要治; 下平 一雄
(Author) Yamamoto, Takeshi; Kurosawa, Yoji; Shimodaira, Kazuo
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-043 (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) Research of combustion technologies to reduce NO(x) emission level of aero engines below 20 percent ...
(言語) jpn(資料番号) AA0063876000
178. Inviscid numerical simulations of 2D parallel blade-vortex interaction JAXA/ONERA cooperation Inviscid numerical simulations of 2D parallel blade-vortex interaction JAXA/ONERA cooperation
(著者名) 田辺 安忠; 齊藤 茂; Yang, Choongmo; ほか
(Author) Tanabe, Yasutada; Saito, Shigeru; Yang, Choongmo; et al.
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-042E (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) Inviscid numerical simulations of two-dimensional parallel blade-vortex interaction are carried out ...
(言語) eng(資料番号) AA0063627000
179. 小型超音速実験機(NEXST-1)飛行実験による空力設計の検証 Demonstration of aerodynamic design technologies on supersonic experimental airplane (NEXST-1) by flight test
(著者名) Kwak, Dong-Youn; 徳川 直子; 吉田 憲司; ほか
(Author) Kwak, Dong-Youn; Tokugawa, Naoko; Yoshida, Kenji; et al.
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-041 (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) Flight test of a supersonic experimental airplane was performed by Japan Aerospace Exploration Agenc...
(言語) jpn(資料番号) AA0063727000
180. 0.44m極超音速衝撃風洞デュアルホイール型模型支持装置環境下の気流偏向特性 Flow-deflection characteristics of JAXA 0.44 m Hypersonic Shock Tunnel with a dual-wheel model support system
(著者名) 山崎 喬; 中北 和之; 中川 宗敬; ほか
(Author) Yamazaki, Takashi; Nakakita, Kazuyuki; Nakagawa, Muneyoshi; et al.
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-06-040 (ISSN) 1349-1113
(刊行年月日) 2007-03-30
(抄録) Flow-deflection characteristic tests were conducted at JAXA 0.44 m Hypersonic Shock Tunnel with a du...
(言語) jpn(資料番号) AA0063796000