AEROSPACE 410 AEROSPACE PROPULSION Lecture ROTARY ENGINES WANKEL ENGINE ROTATING PISTON
PowerPoint Presentation€¦ · PPT file · Web view · 2003-03-06PULSE JET PROPULSION AEROSPACE...
80
Transcript of PowerPoint Presentation€¦ · PPT file · Web view · 2003-03-06PULSE JET PROPULSION AEROSPACE...
AEROSPACE seminar for first year studentsAEROSPACE PROPULSION
Dr. Cengiz CamciProfessor of Aerospace Engineering
Turbomachinery Aero/Heat Transfer LaboratoryP S U Rotorcraft Center of Excellence
http://www.personal.psu.edu/cxc11 QuickTime™ and a
Cinepak decompressorare needed to see this picture.
Faculty teaching and researchingin
PROPULSION RELATED AREAS
Prof. M. MicciAdvanced Rocket Propulsion
Chemical rockets and electric propulsion
Prof. D. LevinHypersonic Flows, Space Environment
Prof. Cengiz CamciHeat Transfer and Fluid Mechanics in Propulsion
Systems
AEROSPACE 410AEROSPACE PROPULSION
Fall 2002
Office HoursM/W/F 1:10 pm-2:30 pm
TEXT:
Mechanics and Thermodynamicsof Propulsion
Hill and Peterson Second edition
(Required)
AEROSPACE 410AEROSPACE 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:Homework 20%Exam 1 25%Exam 2 25%Final exam 30%
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 tothe College of Engineering
guidelineson 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.
IntroductionReview of gas dynamics and thermodynamicsCombustion chemistryCalculating combustion temperaturesGas phase equilibrium
Cycle analysisThrust end efficienciesSubsonic inletsSupersonic inlets Air-breathing engine nozzles
COURSE OUTLINE
Combustion chambers Ramjets and scramjets
Introduction to turbomachineryAxial compressorsSingle stage axial compressorsEfficiency and performanceOff-design performanceRadial variationsThe compressor starting problem
Centrifugal compressorsInducers and diffusersCentrifugal compressor performance
Axial turbinesTurbine performance and designTurbine cooling
Total air-breathing engine performance
Introduction to rocketsWhy multistage?The ideal rocketRocket nozzle analysisRocket nozzle designLiquid rocketsSolid rockets
Review of electricity and magnetism Electric propulsion
Advanced propulsion concepts
PULSE JET PROPULSION
AEROSPACE 410AEROSPACE PROPULSION
Fall 2002
Dr. Cengiz CamciProfessor of Aerospace Engineering
Turbomachinery Aero/Heat Transfer LaboratoryP S U Rotorcraft Center of Excellence
