AE630 : Dynamics of Low Speed Flight

Department

Department of Aeronautical Engineering

Academic Program

Master in Master of Aerospace Engineering

Type

Compulsory

Credits

03

Prerequisite

Overview

Introduction to dynamic stability of flight, static stability theory, requirementsof static stability in pitching motion, full non-linear system of aircraft equations ofmotion, state-space format, possible trends of solution, linearization of the equations and decoupling in to two independent sets, description of forces and moments onaircraft, concept and evaluation of stability derivatives, aircraft free response,characteristics of longitudinal motion, characteristics of lateral-directional motion, andstability boundaries, introduction to handling qualities of aircraft.