Muwanika Jdiobe

Relevant fluid properties; standard atmospheres; mathematical models of flows about bodies. Characteristic parameters of airfoils and wings. Thin airfoil theory and flows about finite wings. Boundary layers. Propeller theory. Supersonic and hypersonic flows about wings and lifting bodies. Drag polars. Power required for level flight. Rate of climb and descent. Steady turns. Maximum range and endurance. Design applications.Prerequisite(s): Grade of 'C' or higher in MATH 2233. Aerospace Engineering majors only.

Relevant fluid properties; standard atmospheres; mathematical models of flows about bodies. Characteristic parameters of airfoils and wings. Thin airfoil theory and flows about finite wings. Boundary layers. Propeller theory. Supersonic and hypersonic flows about wings and lifting bodies. Drag polars. Power required for level flight. Rate of climb and descent. Steady turns. Maximum range and endurance. Design applications.Prerequisite(s): Grade of 'C' or higher in MATH 2233. Aerospace Engineering majors only.

Acoustical analysis and measurement techniques, with emphasis on design applications for noise and vibration control in machinery and in buildings.Prerequisite(s): Graduate standing or consent of instructor.