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Results 41-50 of 50.

41. 低密度アブレータの内部密度分布解析 An Analysis of In-depth Density Disbibution Within A Low Density Ablator
(著者名) 井上, 高広; 奥山, 圭一; 鈴木, 俊之; ほか
(Author) Inoue, Takahiro; Okuyama, Keiichi; Suzuki, Toshiyuki; et al.
(内容記述) Meeting Information: Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. I...
(文献種別) Conference Paper
(刊行物名) 宇宙航行の力学シンポジウム: 平成22年度(Journal Name) Symposium on Flight Mechanics and Astrodynamics: 2010(刊行年月日) 2011-08
(抄録) The in-depth density distribution within a heated ablative specimens is estimated using an X-ray com...
(言語) jpn(資料番号) AA0065106014
42. 超音速矩形インテークのバズ特性に関する風洞実験 Wind tunnel experiment on buzz characteristics of supersonic rectangular intake
(著者名) 八嶋, 治; 宮岡, 諒; 赤塚, 将拓; ほか
(Author) Yashima, Osamu; Miyaoka, Ryo; Akamatsu, Masahiro; et al.
(内容記述) Meeting Information: Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. I...
(文献種別) Conference Paper
(刊行物名) 宇宙航行の力学シンポジウム: 平成22年度(Journal Name) Symposium on Flight Mechanics and Astrodynamics: 2010(ページ) 63-66(刊行年月日) 2011-08
(抄録) 超音速エンジンではインテーク部においてバズと呼ばれる衝撃波の振動現象が発生することが知られている.本研究では,超音速下でのインテークの性能やバズの発生条件を調査することを目的として,超音速風洞にてイン...
(言語) jpn(資料番号) AA0065106017
43. 超軌道速度を持つ再突入宇宙機の定点着地誘導に関する研究 Study on Guidance Control Law for Precision Landing of a Reentry Vehicle with Superorbital Velocity
(著者名) 正田, 浩一; 山田, 哲哉; 上野, 誠也
(Author) Shoda; Yamada, Tetsuya; Ueno, Seiya
(内容記述) Meeting Information: Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. I...
(文献種別) Conference Paper
(刊行物名) 宇宙航行の力学シンポジウム: 平成22年度(Journal Name) Symposium on Flight Mechanics and Astrodynamics: 2010(刊行年月日) 2011-08
(抄録) Lifting flights during reentry are considered as one of the method to reduce total heat flux and loa...
(言語) jpn(資料番号) AA0065106029
44. 二酸化炭素気流中衝撃波背後の発光スペクトル解析 Analysis of emission spectra behind a shock wave in carbon dioxide gas flow
(著者名) 高栁, 大樹; 藤田, 和央
(Author) Takayanagi, Hiroki; Fujita, Kazuhisa
(内容記述) Meeting Information: Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. I...
(文献種別) Conference Paper
(刊行物名) 宇宙航行の力学シンポジウム: 平成22年度(Journal Name) Symposium on Flight Mechanics and Astrodynamics: 2010(刊行年月日) 2011-08
(抄録) The shock tube experiments are carried out to study the radiation behind a strong shock wave in a pu...
(言語) jpn(資料番号) AA0065106013
45. 柔構造エアロシェル大気突入機における形状パラメータの膜面加熱率への影響に関する数値解析 Effects of Shape Parameters on Heating Rate over Aeroshell Membrane for Atmospheric-entry Capsule
(著者名) 渡邉, 保真; 鈴木, 宏二郎; 山田, 和彦
(Author) Watanabe, Yasumasa; Suzuki, Kojiro; Yamada, Kazuhiko
(内容記述) Meeting Information: Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. I...
(文献種別) Conference Paper
(刊行物名) 宇宙航行の力学シンポジウム: 平成22年度(Journal Name) Symposium on Flight Mechanics and Astrodynamics: 2010(刊行年月日) 2011-08
(抄録) An atmospheric-entry capsule needs to endure intense aerodynamic heating during supersonic flight in...
(言語) jpn(資料番号) AA0065106038
46. 火星大気風洞における低レイノルズ数翼型実験 Low Reynolds-Number Airfoil Testing in a Mars Wind Tunnel
(著者名) 浅井, 圭介; 永井, 大樹; 沼田, 大樹; ほか
(Author) Asai, Keisuke; Nagai, Hiroki; Numata, Daijyu; et al.
(内容記述) Meeting Information: Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. I...
(文献種別) Conference Paper
(刊行物名) 宇宙航行の力学シンポジウム: 平成22年度(Journal Name) Symposium on Flight Mechanics and Astrodynamics: 2010(刊行年月日) 2011-08
(抄録) The aerodynamic charactetistics of a 5% flat plate and an NACA0012-34 airfoil in low Reynolds number...
(言語) jpn(資料番号) AA0065106032
47. きぼう利用実験「沸騰二相流体ループにおける気液界面挙動と熱伝達特性」に関するプロジェクト紹介 A Report of a Current Status of an International Space Station "KIBO" Project "Interfacial Behaviors and Heat Transfer Characteristics in Boiling Two Phase Flow"
(著者名) 藤井, 清澄; 川崎, 春夫; 鈴木, 康一; ほか
(Author) Fujii, Kiyosumi; Kawasaki, Haruo; Suzuki, Koichi; et al.
(内容記述) Meeting Information: Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. I...
(文献種別) Conference Paper
(刊行物名) 宇宙航行の力学シンポジウム: 平成22年度(Journal Name) Symposium on Flight Mechanics and Astrodynamics: 2010(刊行年月日) 2011-08
(抄録) Recently, the amount of waste heat in a space facility became larger, because of increase in the spa...
(言語) jpn(資料番号) AA0065106046
48. 低レイノルズ数における薄翼の空力性能評価手法に関する研究 Study on evaluation method for aerodynamic characteristics of thin wing at low Reynolds number
(著者名) 小嶋, 亮次; 李, 東輝; 野々村 拓; ほか
(Author) Kojima, Ryoji; Lee, Dong-Hwi; Nonomura, Taku; et al.
(文献種別) Conference Paper
(刊行物名) 宇宙航行の力学シンポジウム: 平成22年度(Journal Name) Symposium on Flight Mechanics and Astrodynamics: 2010(刊行年月日) 2011-08
(抄録) Abstract :The flow fields around NACA0002 and its aerodynamic characteristics obtained with Three-Di...
(言語) jpn(資料番号) AA0065106033
49. ハイブリッドロケット内部流れの解析に向けた前処理型非定常圧縮性低速流れ: 前処理型流束計算法と3次元流れの影響 Numerical Simulation on Unsteady Compressible Low-Speed Flow Using Preconditioning Method for Hybrid Rocket: Efects of Preconditioning Fluxes and Three-dimensional Flow
(著者名) 坪井, 伸幸; 吹場, 活佳; 嶋田, 徹
(Author) Tsuboi, Nobuyuki; Fukiba, Katsuyoshi; Shimada, Toru
(内容記述) Meeting Information: Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. I...
(文献種別) Conference Paper
(刊行物名) 宇宙航行の力学シンポジウム: 平成22年度(Journal Name) Symposium on Flight Mechanics and Astrodynamics: 2010(刊行年月日) 2011-08
(抄録) Four preconditioned advective upwind splitting methods (AUSM) of low-diffusion flux-splitting scheme...
(言語) jpn(資料番号) AA0065106005
50. 高エンタルピ・高圧気流条件での再突入カプセルの風洞実験 Wind tunnel experiments with re-entry capsule model under high-enthalpy high-pressure flow condition
(著者名) 丹野, 英幸; 小室, 智幸; 佐藤, 和雄; ほか
(Author) Hideyuki, Tanno; Komuro, Tomoyuki; Sato, Kazuo; et al.
(内容記述) Meeting Information: Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. I...
(文献種別) Conference Paper
(刊行物名) 宇宙航行の力学シンポジウム: 平成22年度(Journal Name) Symposium on Flight Mechanics and Astrodynamics: 2010(刊行年月日) 2011-08
(抄録) Aeroheating test with re-entry capsule configuration has carried out in JAXA-HlEST. An Apollo CM 6% ...
(言語) jpn(資料番号) AA0065106012