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Instructors: Prof. Dr.-Ing. Uwe Klingauf
Event type:
Lecture
Org-unit: Dept. 16 - Mechanical Engineering
Displayed in timetable as:
Flight Mech II: Dyn
Subject:
Crediting for:
Hours per week:
3
Language of instruction:
Englisch
Min. | Max. participants:
- | -
Digital Teaching:
The event takes place in person. Further information will be given in the first lecture.
Course Contents:
Aircraft Stability and Dynamics
- static longitudinal motion (lift, pitching moment, neutral point,
manoeuvre point)
- static lateral motion (yaw moments, roll moments, state of flight:
steady sideslip manoeuvre, flight with only one engine, steady turn)
- dynamic longitudinal stability (stability axis system, linearized
equations of motion, Eigenvalues: short period mode, phugoid mode)
- dynamic lateral stability (linearized equations of motion,
Eigenvalues: rolling subsidence mode, spiral convergence/divergence
mode, dutch roll)
Literature:
U. Klingauf: Lecture Script
B. Etkin / L.D. Reid: Dynamics of Flight
R. Brockhaus / W. Alles / R. Luckner: Flugregelung
T. R. Yechout: Introduction to Aircraft Flight Mechanics
B.L. Stevens / F. F. Levis: Aircraft Control and Simulation
J. D. Anderson: Introduction to Flight
M. V. Cook: Flight Dynamic Principles
Preconditions:
Background in engineering mathematics (calculus, lineare algebra und differential equations), technical mechanics (statics and dynamics), fluid mechanics (incompressible flow) and systems theory (multivariable systems and state space) necessary.
Expected Number of Participants:
75
Online Offerings:
moodle
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