AE 550. Dynamics of Flight I. 4 Hours.

Introduction to Tensors Algebra. Frames and coordinates in dynamics systems. General equations of motion of rigid airplanes and reduction to steady state flight situations. Steady state forces and moments. Stability derivatives. Static stability, control and trim. Trim envelope. Relationships with handling quality requirements. Engine-out flight. Effects of the control system. Implications to airplane design. Prerequisite: AE 445 and MATH 220. Corequisite: MATH 290. LEC.

Bachelor of Science in Aerospace Engineering

http://catalog.ku.edu/engineering/aerospace-engineering/bs/

...Design AE 524 Propulsion Systems Design I AE 545 Fundamentals of Aerodynamics 4 AE 550...

Bachelor of Science in Engineering Physics

http://catalog.ku.edu/engineering/engineering-physics/bs/

...3 AE 507 Aerospace Structures I 3 AE 545 Fundamentals of Aerodynamics 4 AE 550...

Bachelor of Science in Mathematics

http://catalog.ku.edu/liberal-arts-sciences/math/bs/

...3 AE 507 Aerospace Structures I 3 AE 545 Fundamentals of Aerodynamics 4 AE 550...