14840 - Aero Engine Design and Analysis 1 Modulübersicht
| Module Number: | 14840 |
| Module Title: | Aero Engine Design and Analysis 1 |
| Flugtriebwerkskonstruktion und -analyse 1 | |
| Department: | Faculty 3 - Mechanical Engineering, Electrical and Energy Systems |
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| Language of Teaching / Examination: | English |
| Duration: | 1 semester |
| Frequency of Offer: | Every summer semester |
| Credits: | 6 |
| Learning Outcome: | At the end of the module the student are able to understand the layout and construction of core engine designs, including compressor and combustion chamber. They are able to evaluate new designs in the field of core engines and to independently propose and develop justified adaptations of standard designs. The independent development of application-related and research-oriented knowledge represents a complementary point of the acquired competence. In general, the students will learn:
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| Contents: | Introduction & Engine Performance
Engine Systems
Compressor
Combustor
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| Recommended Prerequisites: |
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| Mandatory Prerequisites: | No successful completion of module 13802 Core Engine Design 1 |
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| Teaching Materials and Literature: |
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| Module Examination: | Final Module Examination (MAP) |
| Assessment Mode for Module Examination: |
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| Evaluation of Module Examination: | Performance Verification – graded |
| Limited Number of Participants: | None |
| Part of the Study Programme: |
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| Remarks: | This module is previously offered as Core Engine Design 1 |
| Module Components: | Lecture and exam |
| Components to be offered in the Current Semester: |
