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Institution:
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Iowa State University
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Subject:
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Description:
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Cr. 3. F. Prereq : 311. Atmospheric propulsion system performance and cycle analysis. Momentum theorem, thrust and propulsive effi ciency. Thermodynamics of compressible fl ow with heat and work addition. Components and principles of turbojets and turbofans. Rocket engines and ramjet principles. Nonmajor graduate credit.
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Credits:
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0.00 - 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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(515) 294-5836
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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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