Zobrazeno 1 - 10
of 10
pro vyhledávání: '"熱力学的平衡"'
Autor:
佐藤, 吉宣
別途PDFとして添付。ELSEVIER誌掲載論文に関してDOIを記載、Journal of Electrochemical Society 掲載論文に関して、著作権利用許可の一文を追記
0048
甲第19823号
エネ博第329号
新制||エ
0048
甲第19823号
エネ博第329号
新制||エ
Externí odkaz:
http://hdl.handle.net/2433/215649
Autor:
Satou, Yoshinori
別途PDFとして添付。ELSEVIER誌掲載論文に関してDOIを記載、Journal of Electrochemical Society 掲載論文に関して、著作権利用許可の一文を追記
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::c40d1c3f1b4c093e270b4e187cc00e4f
http://hdl.handle.net/2433/215649
http://hdl.handle.net/2433/215649
Publikováno v:
第27回宇宙エネルギーシンポジウム 平成19年度 = The Twenty-seventh Space Energy Symposium. :126-130
A simplified method to compute static temperature using Microsoft Excel is presented in this report. There are two ways for prediction of temperature. One is transient temperature analysis, and the other is steady state analysis. For the thermal desi
Publikováno v:
第27回宇宙エネルギーシンポジウム 平成19年度 = The Twenty-seventh Space Energy Symposium. :49-53
The hybrid solar sail that has the potential to explore the Jupiter and asteroids requires very light weight photovoltaic solar array system with specific power exceeding 1 kW/kg. We expect to reduce the mass of the solar array system dramatically ut
An experimental study of force measurements of blunt cone models in high enthalpy shock tunnel HIEST
Autor:
Sato, Kazuo, Komuro, Tomoyuki, Takahashi, Masahiro, Hashimoto, Tokitada, Tanno, Hideyuki, Ito, Katsuhiro
Publikováno v:
宇宙航空研究開発機構特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency. :99-102
In the present paper, two blunt cone models with 15 degrees of half angle were tested in a high enthalpy shock tunnel to investigate fundamental real gas effect on high enthalpy aerodynamic characteristics. The curvature radius of the tip of model ar
Autor:
Ishibashi, Ko, Ono, Sosuke, Senshu, Hiroki, Sugita, Seiji, Kadono, Toshihiko, Matsui, Takafumi
Publikováno v:
第38回月・惑星シンポジウム = Proceedings of the 38th ISAS Lunar and Planetary Symposium. :17-20
Gaseous species produced within impact-induced vapor clouds may have played an important role in surface environment of planets. However, the molecular composition of those gases is not known well. In particular, interaction between carbon compounds
Autor:
Matsuyama, Shingo, Sawada, Keisuke
Publikováno v:
宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2004論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004. :63-68
A trajectory-based heating analysis of the Galileo probe entry flowfield is attempted to reproduce the heatshield recession data obtained during the entry flight. In the present calculation, the mass conservation equations for the freestream gas (hyd
Publikováno v:
宇宙航行の力学シンポジウム 平成16年度 = Symposium on Flight Mechanics and Astrodynamics 2004. :78-81
資料番号: AA0048089020
Autor:
Sakai, Takeharu
Publikováno v:
宇宙航行の力学シンポジウム 平成15年度 = Symposium on Flight Mechanics and Astrodynamics 2003. :103-106
The entire flowfield within a segmented-constrictor type arc-heated wind tunnel is simulated to numerically characterize the freestream properties produced by the wind tunnel. The flow from the upstream electrode chamber to the nozzle throat is solve
Publikováno v:
宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003. :190-195
A new coupled simulation program for flow and heat conduction has been developed based upon a common CFD platform UPACS. It connects flow calculation blocks and solid blocks without using surface temperature values explicitly. The time-lag between fl