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| Detailed information |
| Original study plan |
Master's programme Mechatronics 2022W |
| Objectives |
After successfully engaging with the topics of this course, students will be able to
- comprehend the derivation of the gas dynamics equation from the basic equations of inviscid, stationary flows,
- apply Prandtl-Glauert transformation to subsonic compressible flows,
- apply Ackeret's Theory to supersonic compressible flows,
- calculate nonliniear effects in supersonic flows (oblique shock waves, expansion fans),
- calculate one-dimensional wave propogation.
The level of mathematical modeling and analysis of the mentioned topics is comparable to the level of the textbooks: Zierep, Theoretische Gasdynamik, 1976 und Anderson, Modern Compressible Flow, 1990.
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| Subject |
- fundamentals of gas dynamics
- compressible subsonic flow
- linear and nonlinear calculation of supersonic flow
- wave propagation
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| Criteria for evaluation |
Written and/or oral exam
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| Methods |
Lecture by means of a script
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| Language |
German |
| Study material |
- K. Oswatitsch: Grundlagen der Gasdynamik, Springer, Berlin, 1976.
- J. Zierep: Theoretische Gasdynamik, Braun, Karlsruhe, 1976.
- J.D. Anderson: Modern Compressible Flow, McGraw-Hill, 1990.
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| Changing subject? |
No |
| Further information |
Accompanying tutorial course
Until term 2022S known as: 481WTMKSM2V12 VL Fluid Dynamics 2
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| Corresponding lecture |
(*)ME3WNVOSME2: VO Strömungsmechanik II (Reibungsströmungen, Gasdynamik) (3 ECTS) oder
MEMWHVOSMKM: VO Strömungsmechanik kompressibler Medien (3 ECTS)
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| Earlier variants |
They also cover the requirements of the curriculum (from - to)
481WTMKSM2V12: VL Fluid Dynamics 2 (2012W-2022S)
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