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Institution:
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Western Michigan University
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Subject:
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Description:
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An introduction to compressible aerodynamics and boundary layer theory, including subsonic and supersonic flows over wings and bodies and viscous flows. Emphasis is placed on application of the basic theory for solving practical aerodynamic problems in the design of flight vehicles. Prerequisites & Corequisites: Prerequisites: AAE 3610; MATH 3740; ME 2580. Credits: 3 hours
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Credits:
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3.00
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Credit Hours:
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Prerequisites:
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Corequisites:
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Exclusions:
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Level:
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Instructional Type:
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Lecture
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Notes:
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Additional Information:
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Historical Version(s):
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Institution Website:
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Phone Number:
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(269) 387-1000
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Regional Accreditation:
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North Central Association of Colleges and Schools
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Calendar System:
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Semester
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