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
Voraussetzungen: Grundlagen der Flugtechnik
Performance assessment
Performance assessment information (valid until the course unit is held again)