授業情報/Course information

開講学期/Course Start 2019年度/Academic Year  前期/First
開講曜限/Class period 水/Wed 1,水/Wed 2
授業区分/Regular or Intensive 週間授業
対象学科/Department 生産システム工学系専攻航空宇宙総合工学コース
対象学年/Year 1年
授業科目区分/Category 博士前期課程 大学院自専攻科目
必修・選択/Mandatory or Elective 選択
授業方法/Lecture or Seminar 講義科目
授業科目名/Course Title 航空宇宙流体機械工学特論(英語希望留学生専用)
単位数/Number of Credits 1.0
担当教員名/Lecturer 今井良二
時間割コード/Registration Code MQ217E
連絡先/Contact 今井良二(5336)
オフィスアワー/Office hours 今井良二(水曜日15:00-17:00)
実務経験/Work experience 今井良二(輸送用機器製造事業を扱う企業での航空推進システムの流体設計技術の開発及び航空宇宙推進システム、原子力、エネルギープラント関連機器の伝熱設計技術の開発経験を有する)
更新日/Date of renewal 2019/02/10
授業のねらい
/Learning Objectives
This course aims to provide general understanding of principles and design method for aerospace turbo machinery, such as turbo pump. This course includes following aspects: (1) Hydro thermodynamics and design method of turbo machines including structural aspects and material selection, (2) Cavitation and related problems in turbo pump, (3) Computational fluid dynamics in turbo pump (4) Instability phenomena in turbo machines, (5) Future prospects.
到達度目標
/Outcomes Measured By:
1. To develop understanding of general principle of turbine, compressor, and turbine.
2. To develop understanding of related problem and future prospect in order to make a new research proposal. "
授業計画
/Course Schedule
1. Thermal and hydraulics of turbo machinery (1)
2. Thermal and hydraulics of turbo machinery (2)
3. Design method of turbo pump
4. Cavitation and bubble dynamics
5. CFD in turbo pump
6. Instability problem (No. 1)
7. Instability problem (No. 2)
I recommend to read reference book and paper even outside a school hour in order to obtain deep understanding."
参考書等
/Required Materials
ガスタービンエンジン 谷田好通, 長島利夫著 朝倉書店 2000(ISBN:4254230974)
流体機械 大橋秀雄著 森北出版 1987流体機械 大橋秀雄著 森北出版 1987(ISBN:4627621817)
ポンプの流体力学 Christopher E. Brennen著 ; 辻本良信訳 大阪大学出版会 1998(ISBN:4872590368)
Cavitation and bubble dynamics Christopher Earls Brennen Cambridge University Press 2014(ISBN:9781107644762)
Elements of propulsion : gas turbines and rockets Jack D. Mattingly ; foreword by Hans von Ohain American Institute of Aeronautics and Astronautics 2006(ISBN:1563477793)
成績評価方法
/Grading Guidelines
The score of each student is evaluated by report and attendance. A grade of more than 60% is accepted for a credit.
履修上の注意
/Notices
Basically understandings for fluid dynamics, thermodynamics, and heat transfer engineering are required for this subject.
教員メッセージ
/Message from Lecturer
Turbo machineries are main components of jet engine and rocket engine system. This subject aims to develop understandings of turbo machinery system through basic principle of turbo machines.
学習・教育目標との対応
/Learning and Educational Policy
Target of this subject corresponds to following items described as aims of learning and education in this course:
1. Development of ability one can analyze and evaluate a basic key technology which constitutes system
2. Development of ability one can integrate some elemental technologies and evaluate as system
"

備考
/Notes
This subject will be taught in English.
No. 回(日時)
/Time (date and time)
主題と位置付け(担当)
/Subjects and instructor's position
学習方法と内容
/Methods and contents
備考
/Notes
該当するデータはありません
Active learning 1-1
/主体的学修(反転授業,小テスト,振り返り 等)
広範でかつ高度な実践的授業ですから、調査や検討を授業進捗にあわせて自ら学習すること。 レポートを宿題とすることがあります。
Active learning 1-2
/上記項目に係るALの度合い
15%~50%
Active learning 2-1
/対話的学修(グループ学習,協働,調査体験 等)
Active learning 2-2
/上記項目に係るALの度合い
該当なし
Active learning 3-1
/深い学修(複数科目の知識の総合化や問題解決型学修 等)
Active learning 3-2
/上記項目に係るALの度合い
該当なし