AERO ENG 271 - Aerodynamics II

Institution:

Missouri University of Science and Technology

Subject:

Aerospace Engineering

Description:

Three dimensional incompressible wing theory. Compressible one dimensional flow with normal and oblique shock waves, heat addition, and friction. Compressible transonic, and supersonic linearized flow theory. Supersonic wings and wing/fuselage configurations. Prerequisite: "C" or better in Aero Eng 231 and Mech Eng 219.

Credits:

3.00

Credit Hours:

Prerequisites:

Corequisites:

Exclusions:

Level:

Instructional Type:

Lecture

Notes:

Additional Information:

Historical Version(s):

Institution Website:

www.mst.edu/

Phone Number:

(573) 341-4111

Regional Accreditation:

North Central Association of Colleges and Schools

Calendar System:

Semester

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