Equations of motion. Aircraft flight perfomance, flight envelope. Aircraft static stability and control, longituadinal and lateral stbility. Dynamic longitudinal and lateral stability. Flight test. Wind tunnel test.
Objective
- Knowledge of methods to solve flight mechanic problems - To be able to apply basic methods for flight performence calculation and stability investigations - Basic knowledge of flight and wind tunnel tests and test evaluation methods
Content
Equations of motion. Aircraft flight perfomance, flight envelope. Aircraft static stability and control, longituadinal and lateral stbility. Dynamic longitudinal and lateral stability. Flight testing. Wind tunnel testing.
Lecture notes
Ausgewählte Kapitel der Flugtechnik (J. Wildi)
Literature
Mc Cormick, B.W.: Aerodynamics, Aeronautics and Flight Mechanics (John Wiley and Sons), 1979 / 1995
Anderson, J: Fundamentals of Aerodynamics (McGraw-Hill Comp Inc), 2010
Prerequisites / Notice
Recommended: Lecture 'Basics of Aircraft und Vehicle Aerodynamics' (FS)
Performance assessment
Performance assessment information (valid until the course unit is held again)
The performance assessment is offered every session. Repetition possible without re-enrolling for the course unit.
Mode of examination
written 90 minutes
Additional information on mode of examination
Es sind Verständnisfragen schriftlich zu beantworten. Dabei sind je nach Aufgabe qualitative und/oder quantitative Antworten möglich. Technisch-wissenschaftlicher Taschenrechner (ohne Internet-Zugang) erforderlich.
Written aids
Skript "Grundlagen der Flugtechnik" und Skript "Ausgewählte Kapitel der Flugtechnik" sowie Übungsunterlagen Selbst erstellte Zusammenfassung / Notizen / Vorlesungsunterlagen Technisch-wissenschaftlicher Taschenrechner (ohne Internet-Zugang) erforderlich
This information can be updated until the beginning of the semester; information on the examination timetable is binding.
Learning materials
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Only public learning materials are listed.
Groups
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Restrictions
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