JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

JAXA Publication series

Search by Category

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

Results 121-140 of 351.

previous 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 next
121. A parametric study on parallel blade-vortex interaction for helicopter rotor A parametric study on parallel blade-vortex interaction for helicopter rotor
(著者名) 田辺 安忠; 齊藤 茂; 高崎 啓介; ほか
(Author) Tanabe, Yasutada; Saito, Shigeru; Takasaki, Keisuke; 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-07-051E (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) A parametric study on parallel Blade-Vortex Interaction (BVI) is carried out. A high accuracy CFD (C...
(言語) eng(資料番号) AA0063918000
122. 超音速機高揚力装置に関する数値解析及び考察 Numerical investigation of supersonic transport high-lift devices
(著者名) Lei, Zhong
(Author) Lei, Zhong
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-050 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) Flow field around a configuration of supersonic transport with high-lift devices at low speed and hi...
(言語) jpn(資料番号) AA0063943000
123. Adjoint感度解析を用いた勾配法による空力形状最適設計 Aerodynamic shape design using gradient-based optimization with adjoint sensitivity analysis
(著者名) Lei, Zhong; 牧野 好和; 岩宮 敏幸
(Author) Lei, Zhong; Makino, Yoshikazu; Iwamiya, Toshiyuki
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-049 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) This paper describes an optimization design technology and some applications of CFD (Computational F...
(言語) jpn(資料番号) AA0063996000
124. コックピット・ワークロード推算プログラムの開発 Development of flightcrew workload estimation package
(著者名) 津田 宏果; 村岡 浩治; 稲田 崇志; ほか
(Author) Tsuda, Hiroka; Muraoka, Koji; Inada, 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-07-048 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) JAXA developed a software package; FWEP (Flightcrew Workload Estimation Package) which can be used i...
(言語) jpn(資料番号) AA0064016000
125. 極超音速機のマッハ5空力特性試験 Mach 5 wind tunnel test of hypersonic airplane
(著者名) 田口 秀之; 藤田 和央; 進藤 重美; ほか
(Author) Taguchi, Hideyuki; Fujita, Kazuhisa; Shindo, Shigemi; 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-07-047 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) Mach 5 aerodynamic coefficients for a hypersonic experimental airplane are examined at JAXA 0.5 m hy...
(言語) jpn(資料番号) AA0063912000
126. 航空機地上走行モデルの高度化 Advanced aircraft ground-roll model
(著者名) 新川 智子; 舩引 浩平; 野嶋 琢也; ほか
(Author) Shinkawa, Tomoko; Funabiki, Kohei; Nojima, Takuya; 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-07-046 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) As a part of cooperative research program between Japan Aerospace Exploration Agency and Mitsubishi ...
(言語) jpn(資料番号) AA0063995000
127. 半導体レーザ吸収法によるExpansion Tube気流の計測 Expansion tube flow diagnostics using laser diode absorption spectroscopy
(著者名) 中北, 和之
(Author) Nakakita, Kazuyuki; Jeffries, Jay B.; Hanson, Ronald K.
(内容記述) 形態: カラー図版あり
(文献種別) Technical Report (レポート番号) JAXA-RR-07-045 (ISSN) 1349-1113
(刊行物名) 宇宙航空研究開発機構研究開発報告(Journal Name) JAXA research and development report(巻) JAXA-RR-07-045(刊行年月日) 2008-02-29
(抄録) An expansion tube flow diagnostics was conducted to identify its flow static temperature as a resear...
(言語) jpn(資料番号) AA0064227000
128. 1軸ターボジェットエンジンのオンライン性能推定試験 On-line performance estimation tests of single spool turbojet engines
(著者名) 田頭 剛; 水野 拓哉; 高 將治; ほか
(Author) Tagashira, Takeshi; Mizuno, Takuya; Ko, Masaharu; 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-07-044 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) On-line performance estimation is important for the future advanced control systems of jet engines. ...
(言語) jpn(資料番号) AA0063942000
129. 米国CAPSTONEプログラムへの参加による次世代運航システムの評価飛行実験 Fligyt test evaluation of the CAPSTONE advanced aircraft operation systems
(著者名) 奥野, 善則; 舩引, 浩平; 野嶋, 琢也; ほか
(Author) Okuno, Yoshinori; Funabiki, Kohei; Nojima, Takuya; et al.
(内容記述) 形態: カラー図版あり
(文献種別) Technical Report (レポート番号) JAXA-RR-07-043 (ISSN) 1349-1113
(刊行物名) 宇宙航空研究開発機構研究開発報告(Journal Name) JAXA research and development report(巻) JAXA-RR-07-043(刊行年月日) 2008-02-29
(抄録) Flight test evaluations of the CAPSTONE advanced aircraft operation systems have been conducted by J...
(言語) jpn(資料番号) AA0064346000
130. 燃焼合成における燃焼波伝播および自己着火に関する機構解明ツールの検証: Ti-Al系への適用 Evaluation of analytical tools for exploring mechanisms of flame propagation and/or ignition in materials synthesis by combustion: Application to Ti-Al system
(著者名) 牧野 敦
(Author) Makino, Atsushi
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-042 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) In order to elucidate combustion mechanisms, such as those for flame propagation and/or ignition of ...
(言語) jpn(資料番号) AA0063911000
131. 液糸からの液滴分裂における伝播性表面張力波の作用の解明に関する数値解析 A numerical study on the role of propagative capillary waves in droplet formation from a ligament
(著者名) 新城 淳史; 松山 新吾; 溝渕 泰寛; ほか
(Author) Shinjo, Junji; Matsuyama, Shingo; Mizobuchi, Yasuhiro; 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-07-041 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) A novel understanding of droplet formation mechanism from a ligament is presented. In the scaled-up ...
(言語) jpn(資料番号) AA0063887000
132. 振動ピンを用いた皮膚感覚呈示装置によるパイロットへの飛行情報呈示に関する研究 A study on pilot flight display using pin-array-type tactile display
(著者名) 野嶋 琢也; 舩引 浩平
(Author) Nojima, Takuya; Funabiki, Kohei
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-040 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) When flying aircraft, it is required for pilots to watch outside and flight instruments inside caref...
(言語) jpn(資料番号) AA0063994000
133. 飛行データ解析プログラムのための乗員行動再構築 Flight crew task reconstruction for Flight Data Analysis program
(著者名) 村岡 浩治; 津田 宏果
(Author) Muraoka, Koji; Tsuda, Hiroka
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-039 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) The Japan Aerospace Exploration Agency (JAXA) has started development of a proactive flight crew ope...
(言語) jpn(資料番号) AA0063993000
134. ヘリコプタ騒音低減用アクティブ・タブの研究 Research activities of Active Tab for helicopter noise reduction
(著者名) 小曳 昇; 齊藤 茂; 青山 剛史; ほか
(Author) Kobiki, Noboru; Saito, Shigeru; Aoyama, 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-07-038 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) This paper presents the activities of Active Tab joint research/development program and the experime...
(言語) jpn(資料番号) AA0063992000
135. ホットフィルムを用いた超音速小型実験機の遷移計測 Transition measurement using hot-film on supersonic experimental airplane NEXST-1
(著者名) 徳川 直子; 吉田 憲司
(Author) Tokugawa, Naoko; Yoshida, Kenji
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-037 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) Boundary layer transition on natural laminar flow wing is measured using hot-film and other three ki...
(言語) jpn(資料番号) AA0064087000
136. 非定常圧力トランスデューサーを用いた超音速小型実験機の遷移計測 Transition measurement using dynamic pressure transducer on supersonic experimental airplane NEXST-1
(著者名) 徳川 直子; 吉田 憲司
(Author) Tokugawa, Naoko; Yoshida, Kenji
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-036 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) Boundary layer transition on natural laminar flow wing is measured using dynamic pressure transducer...
(言語) jpn(資料番号) AA0064086000
137. 流体・壁面後退量連成解析によるノズル壁後退量評価 Estimation of recession amount of nozzle wall using coupled fluid/thermochemical approach
(著者名) 大門 優; 嶋田 徹; 坪井 伸幸; ほか
(Author) Daimon, Yu; Shimada, Toru; Tsuboi, Nobuyuki; 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-07-035 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) Evaluation of ablation of nozzle wall in solid rocket motor is studied numerically on three solid ro...
(言語) jpn(資料番号) AA0063804000
138. Thermal zero shift correction of strain-gage balance output in the JAXA 2 m x 2 m Transonic Wind Tunnel 2m×2m遷音速風洞における天秤温度ドリフト補正方法
(著者名) 香西 政孝; 塩原 辰郎; 上野 真; ほか
(Author) Kozai, Masataka; Shiohara, Tatsuro; Ueno, Makoto; 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-07-034E (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) In the JAXA 2 m x 2 m Transonic Wind Tunnel, the thermal zero shift of strain-gage balance output ca...
(言語) eng(資料番号) AA0063886000
139. パネル法による遷音速風洞境界修正法の開発 Wall interference correction by the panel method for the JAXA 2 m x 2 m transonic wind tunnel
(著者名) 日高 亜希子; 口石 茂; 小池 陽; ほか
(Author) Hidaka, Akiko; Kuchiishi, Shigeru; Koike, Akira; 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-07-033 (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) In the JAXA transonic wind tunnel, some wall interference correction methods were investigated in th...
(言語) jpn(資料番号) AA0063885000
140. The stacking method: The technique to detect small size of GEO debris and asteroids 重ね合わせ法:微小静止デブリ及び小惑星の検出法
(著者名) 柳沢 俊史; 黒崎 裕久; 中島 厚
(Author) Yanagisawa, Toshifumi; Kurosaki, Hirohisa; Nakajima, Atsushi
(内容記述) JAXA Research and Development Report
(文献種別) Technical Report (レポート番号) JAXA-RR-07-032E (ISSN) 1349-1113
(刊行年月日) 2008-02-29
(抄録) We established a new method that we call 'the stacking method' to detect faint objects on CCD (Charg...
(言語) eng(資料番号) AA0063910000