Výsledky vyhledávání - "Matsukawa, Yutaka"

Assessment of Vibrational Transition Models for Nonequilibium High Temperature Flows: Collinear Collision QCT Model

Autor: Matsukawa, Yutaka

Publikováno v: 宇宙航行の力学シンポジウム: 平成22年度 = Symposium on Flight Mechanics and Astrodynamics: 2010. :57-62

宇宙航行の力学シンポジウム平成22年度 (2010年12月16-17日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県
Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. Institute

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8f4d099b904d0d7671264b38b161453f
http://id.nii.ac.jp/1696/00014329/

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Assessment of Vibrational Transition Rate Coefficient Models for High Temperature Reentry Flows

Autor: Matsukawa, Yutaka

Publikováno v: 宇宙航行の力学シンポジウム: 平成21年度 = Symposium on Flight Mechanics and Astrodynamics: 2009. :137-140

平成21年度宇宙航行の力学シンポジウム（2009年12月10日-11日. 宇宙航空研究開発機構宇宙科学研究本部）, 相模原市, 神奈川県
Symposium on Flight Mechanics and Astrodynamics 2008 (December 10-11, 2009. In

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2a6e15831ed41dcd284231d4a9e9c63d
http://id.nii.ac.jp/1696/00014400/

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Analytical evaluation of the solid rocket motor nozzle surface recession by the alumina-carbon reaction

Autor: Matsukawa, Yutaka, Sato, Yutaka

Publikováno v: 宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling. :168-174

A theoretical model describing the chemical ablation of a solid rocket motor nozzle ablator by the alumina-carbon reaction is presented. An application of it to a typical solid rocket motor with a graphite nozzle ablator indicates a large influence o

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e3819afaadf4de8a2e5d82196facccad
http://id.nii.ac.jp/1696/00005666/

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Technology improvement in assessment of planetary entry environments and prediction of thermal protection system performance

Autor: Fujita, Kazuhisa, Matsuyama, Shingo, Suzuki, Toshiyuki, Matsukawa, Yutaka

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. :103-106

Comprehensive researches on high-enthalpy flows and associated thermal protection technologies have been conducted in Aerodynamic Research Group, IAT, in cooperation with other research groups in JAXA. In this article, an over-view and the current st

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::5ba721af934d139484dcd4b7ba2ab46a
http://id.nii.ac.jp/1696/00006000/

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Study for Dynamically Unstable Motion of Reentry Capsule

Autor: Abe, Takashi, Sato, Syunichi, Matsukawa, Yutaka, Yamamoto, Kazushi, Hiraoka, Kazumi

Publikováno v: The Institute of Space and Astronautical Science report. S.P. : Aerodynamics, Thermophysics, Thermal Protection, Flight System Analysis and Design of Asteroid Sample Return Capsule. 17:301-332

The dynamic stability of the reentry capsule configuration was investigated both experimentally and numerically. The dynamically unstable behavior was observed especially at transonic regime while, at subsonic regime, an intermittent unstable behavio

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9be80106d2f32c896d85b34fcd3e673a
http://id.nii.ac.jp/1696/00033252/

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