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Instantaneous view of the flow field
behind a heated circular cylinder. Flow is from left to right. The flow
vizualization is done with liquid crystal particles, that change their color
according the to temperature they sense. Specifically, the coldest
temperatures reflect blue, and as the temperature increases, the colors of
the liquid crystal change from blue to cyan to green to yellow to orange, and
finally to red, at its hottest temperatures. This picture is from
"Digital Particle Image Velocimetry/Thermometry and Applications to the
Wake of a Heated Circular Cylinder" by Park, Dabiri, & Gharib,
Experiments in Fluids, Vol 30, pp. 327-338
Other interesting images can be found at http://www.efluids.com/efluids/pages/gallery.htm
Department of Aeronautics &
Astronautics
AA
419: Aerospace Heat Transfer
Winter 2008
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Description
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Course
Objectives
Develop the fundamentals of conductive, convective, and radiateive heat
transfer with emphasis on applications to atmospheric and space flight.
1. Understand fundamental concepts of conduction, convection, and radiation
heat transfer and heat transfer with phase change.
2. Develop competence in calculating the heat transfer and/or temperature
distributions in common basic aerospace structural components such as
plates, spheres, cylinders, as well as more complicated configurations such
as surface cooling fins.
3. Develop skills in modeling thermal and heat transfer characteristics of
aerospace systems, such as high-speed aircraft surfaces, combustion
chambers, rocket nozzles, and spacecraft.
4. Use software program of choice (MATLAB, C++, PowerPoint, Photoshop,
CorelDraw, etc.) to design and present.
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Schedule
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· Lectures : MWF
9:30-10:20am (Guggenheim Hall 204)
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Instructor
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Prof.
Dana Dabiri, dabiri@aa.washington.edu
Guggenheim Hall 314 C, (206) 543-6067
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TA
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Eric
Schwerdt, schwee15@u.washington.edu
Guggenheim Hall 306
Office hours : Th 9:30-10:30
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Textbook
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Incropera
& DeWitt, Fundamentals of Heat and Mass Transfer, 5th Edition,
2005
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