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AEROSPACE seminar for first year students AEROSPACE PROPULSION Dr. Cengiz Camci

AEROSPACE seminar for first year students AEROSPACE PROPULSION Dr. Cengiz Camci Professor of Aerospace Engineering Turbomachinery Aero/Heat Transfer Laboratory P S U Rotorcraft Center of Excellence. Coordinates 223 Hammond Building cxc11@psu.edu 814 865 9871 ROOM 41

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AEROSPACE seminar for first year students AEROSPACE PROPULSION Dr. Cengiz Camci

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  1. AEROSPACE seminar for first year students AEROSPACE PROPULSION Dr. Cengiz Camci Professor of Aerospace Engineering Turbomachinery Aero/Heat Transfer Laboratory P S U Rotorcraft Center of Excellence

  2. Coordinates 223 Hammond Building cxc11@psu.edu 814 865 9871 ROOM 41 ROOM 45 ROOM 47 ROOM 8

  3. http://www.personal.psu.edu/cxc11

  4. Faculty teaching and researching in PROPULSION RELATED AREAS • Prof. M. Micci • Advanced Rocket Propulsion • Chemical rockets and electric propulsion • Prof. D. Levin • Hypersonic Flows, Space Environment • Prof. Cengiz Camci • Heat Transfer and Fluid Mechanics in Propulsion Systems

  5. AEROSPACE 410 AEROSPACE PROPULSION Fall 2002 Office Hours M/W/F 1:10 pm-2:30 pm

  6. TEXT: Mechanics and Thermodynamics of Propulsion Hill and Peterson Second edition (Required)

  7. 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.

  8. GRADING: Homework 20% Exam 1 25% Exam 2 25% Final exam 30% 100%

  9. 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.

  10. 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.

  11. COURSE OUTLINE Introduction Review of gas dynamics and thermodynamics Combustion chemistry Calculating combustion temperatures Gas phase equilibrium Cycle analysis Thrust end efficiencies Subsonic inlets Supersonic inlets Air-breathing engine nozzles

  12. Combustion chambers • Ramjets and scramjets • Introduction to turbomachinery • Axial compressors • Single stage axial compressors • Efficiency and performance • Off-design performance • Radial variations • The compressor starting problem

  13. Centrifugal compressors • Inducers and diffusers • Centrifugal compressor performance • Axial turbines • Turbine performance and design • Turbine cooling • Total air-breathing engine performance

  14. 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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