units
MAE3404
Faculty of Engineering
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6 points, SCA Band 2, 0.125 EFTSLRefer to the specific census and withdrawal dates for the semester(s) in which this unit is offered.
SynopsisThis unit introduces the student to the principal areas of aerospace dynamics: atmospheric, transitional, and space flight dynamics. The role of aerodynamic forces acting on an aircraft leads to the development of the equations describing static longitudinal stability, as well as lateral and directional stability. These ideas are extended to consider vehicles transitioning from atmospheric to space travel; atmospheric models, gravitational fields and the kinematics and dynamics of motion in transitional flight are considered, as are the dynamics of atmospheric re-entry. Finally orbital manoeuvres, ballistic, and inter-planetary trajectories are considered. Objectives
Knowledge of the dynamic forces acting on a flight vehicle in different flight environments, and an awareness of the use of equations governing dynamics in the design and use of flight vehicles in industry. Assessment
Practice class/laboratories: 10% Chief examiner(s)Contact hoursSix hours of contact time per week (usually 3 hours lectures and 3 hours practice sessions or laboratories) and 6 hours of private study per week Prerequisites |