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

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Presentation transcript:

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

Coordinates 223 Hammond Building ROOM 41 ROOM 47 ROOM 8

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

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

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

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.

GRADING: Homework20% Exam 125% Exam 225% Final exam30% 100%

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.

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 and clicking on “Student Information” and then “Current Students” on the subsequent menu.

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 COURSE OUTLINE

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

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