AEROSPACE PROPULSION Dr. Cengiz Camci AEROSPACE 410 Fall 2002

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Presentation transcript:

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

cxc11@psu.edu Coordinates 223 Hammond Building 814 865 9871 ROOM 41

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

Monday/Wednesday/Friday AEROSPACE 410 AEROSPACE PROPULSION Fall 2002 Monday/Wednesday/Friday 060 Willard 12:20 pm - 1:10 pm

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

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

AEROSPACE PROPULSION Course Objectives: AEROSPACE 410 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.

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

Tests will be closed book and notes with an equation sheet provided 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.

the College of Engineering guidelines 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.

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

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

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

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