AEROSPACE 410

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AEROSPACE 410 AEROSPACE PROPULSION Fall
2002 Dr. Cengiz Camci Professor of Aerospace
Engineering Turbomachinery Aero/Heat Transfer
Laboratory P S U Rotorcraft Center of
Excellence
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Coordinates 223 Hammond Building cxc11_at_psu.ed
u 814 865 9871 ROOM 41 ROOM 47 ROOM 8
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http//www.personal.psu.edu/cxc11
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AEROSPACE 410 AEROSPACE PROPULSION Fall 2002
Monday/Wednesday/Friday 060 Willard 1220 pm -
110 pm
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AEROSPACE 410 AEROSPACE PROPULSION Fall 2002
Office Hours M/W/F 110 pm-230 pm
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TEXT Mechanics and Thermodynamics of
Propulsion Hill and Peterson Second
edition (Required)
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AEROSPACE 410 AEROSPACE PROPULSION
Course Objectives Upon the completion of this
course students will have the ability to predict
the performance and conduct preliminary design of
aerospace propulsion systems and their
components.
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GRADING Homework 20 Exam 1 25 Exam
2 25 Final exam 30 100
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Tests will be closed book and notes with an
equation sheet provided. Students are allowed to
work together on the homework. However, the
purpose of the homework is to prepare you for the
exams. Thus copying your homework from others
will hurt you on the exams and not doing the
homework altogether will hurt doubly.
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Cheating during exams will not be tolerated and
will be handled according to the College of
Engineering guidelines on academic integrity.
These can be found at the URL address
www.engr.psu.edu and clicking on Student
Information and then Current Students on the
subsequent menu.
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COURSE OUTLINE
Introduction Review of gas dynamics and
thermodynamics Combustion chemistry Calculati
ng combustion temperatures Gas phase
equilibrium Cycle analysis Thrust end
efficiencies Subsonic inlets Supersonic
inlets Air-breathing engine nozzles
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Combustion chambers Ramjets and
scramjets Introduction to turbomachinery Ax
ial compressors Single stage axial
compressors Efficiency and performance Off-design
performance Radial variations The compressor
starting problem
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Centrifugal compressors Inducers and
diffusers Centrifugal compressor performance
Axial turbines Turbine performance and
design Turbine cooling Total air-breathing
engine performance
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Introduction to rockets Why
multistage? The ideal rocket Rocket
nozzle analysis Rocket nozzle design Liquid
rockets Solid rockets Review of
electricity and magnetism Electric
propulsion Advanced propulsion concepts

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AEROSPACE 410 AEROSPACE PROPULSION Fall
2002 Dr. Cengiz Camci Professor of Aerospace
Engineering Turbomachinery Aero/Heat Transfer
Laboratory P S U Rotorcraft Center of
Excellence
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