Dynamics III

Mechanical systems


Contents

The lecture Mechanical Systems - Dynamics III expands particular parts of the previous curriculum Structural Dynamics - Dynamics I and II. A major focus of the course is formed by the damping matrix in general form and further, previously untreated components of the differential equation for linear vibrations of multi-degree-of-freedom systems.  Superordinate aspects such as system stability, identification, and model reduction are also considered:

  • general system aspects,
  • material models and damping,
  • complex vibration modes,
  • mass dampers,
  • modal analysis,
  • gyroscopic und zirkulatory forces,
  • model reduction.

The aim of the lecture is to expand the methodological repertoire for the treatment of vibration problems. On the one hand, this specifically concerns the origin and effect of damping. On the other hand, a general understanding of dynamic systems should be achieved. This facilitates to establish a connection to other areas, such as for example experimetal methods, control theory, flight mechanics and adaptive structures.

Eigenvalue distribution and phase portraits of a linear system with one degree of freedom
Eigenvalue distribution and phase portraits of a linear system with one degree of freedom
00:03
© Deutsches SOFIA Institut

 Vibration mode of the SOFIA telescope from experimental identification

Lecturer:
Weekly amount:

Semester frequency:
Target group:
Prerequisites:

Jörg F. Wagner
2 h lectures (in German)
1 h additional exercises (optional)
Every winter semester or upon request
Master students of Aerospace Engineering as of 2nd sem.
Structural Dynamics - Dynamics I and II,
Flight mechanics, basics of control theory

Current C@MPUS-Link

Semester:WS 24/25
Content:siehe Modulhandbuch
Number:393410000
Type:Lecture
Sh:2
Link:C@MPUS
Organisation:Flugmesstechnik

Contact

 

Chair of Flight Measuring Technology

Pfaffenwaldring 31, D-70569 Stuttgart

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