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Syllabus
Goals
1. Understand the effects of compressibility
2. Use analytical, computational and experimental tools to study compressible
aerodynamics
3. Design airfoils and nozzles for compressible flow
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Course Outcomes
1. The student will understand the effects of compressibility on fluid
flow
2. The student will be able to solve problems with shock waves and expansions
3. The student will be able to solve one-dimensional, compressible flow
problems
4. Student groups will be able to calculate the performance of supersonic
airfoils
5. Students groups will be able to design a supersonic nozzle
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ABET a-k criteria satisfied by this course
a) an ability to apply knowledge of
mathematics, science, and engineering
b) an ability to design and conduct experiments, as well as to analyze and
interpret data
c) an ability to design a system, component, or process to meet desired needs
e) an ability to identify, formulate, and solve engineering problems
g) an ability to communicate effectively
k) an ability to use the techniques, skills, and modern engineering tools
necessary for engineering practice.
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Grading
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Homework:
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~25%
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Midterm:
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~30-35%
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Final:
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~40-45%
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Unless pre-approval is
obtained, penalty for late submission of HW: 50% reduction for 24 hr delay, 100%
reduction for 48hr delay.
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Homework Policy
Homework is due by 8:30 A.M.
on the due date to Brian.
Brian must be
notified in advance if this deadline cannot be made. Late homeworks will be
graded with a lower maximum score.
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Text
Anderson, John D., "Fundamentals of Aerodynamics," 4th Ed.,
McGraw-Hill, 2005.
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Schedule
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Date
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Jan. 7
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Class Begins
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Jan. 10
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No Tutorial
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Jan. 21
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No class MLK Day
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Feb 15
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Midterm Exam
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Feb 18
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No Class Presidents Day
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Mar 14
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Class ends
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Mar 19
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8:30-10:20 am Final Exam
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