by Dr. Ian Halliwell, Northwind Propulsion Inc.
ü This 32-hour course introduces GasTurb14 through software demonstration, complete engine model generations, simulations, and optional homework assignments.
ü All students will receive an AIAA Certificate of Completion at the end of the course
OVERVIEW
Gas turbine performance – usually over a specific mission or commercial route for a particular aircraft – is what engine manufacturers sell. Therefore, it is very important that we define and quantify performance clearly and unambiguously. High thrust and low fuel burn throughout the mission rank highly on the list of performance requirements but engine mass and complexity influence marketability very significantly on account of purchase price and operating costs. Prevailing temperatures of the hot components affect component lives very significantly, so the engine cycle selected at the design point is critical. Preliminary engine design and performance are linked inextricably. If incorrect decisions are made in the early stages of a new engine program, the best CFD in the world will not save the project!
“A Practical Approach to Gas Turbine Engine Performance & Design using GasTurb14” is a 32-hour AIAA Short Course, delivered in sixteen 2-hour sessions, presents:
- an introduction to the overall performance of gas turbine engines used for aircraft propulsion
- the contribution of each major flowpath component to complete engine performance
- the use of appropriate trade studies to optimize design and performance choices
- the structured development of an approach to the generation of engine performance models, with component masses and geometries, all based on GasTurb14 software, for which licenses and a User Guide will be provided
The course materials provided will cover all appropriate theory but will frequently be used only for reference and use between classes. Emphasis will be given to the demonstration of the software and its subsequent use by course participants:
- an introduction to GasTurb14 will occur early in the workshop
- the generation of complete engine models will be illustrated and be the topic of trade studies as homework between sessions
- a recent topic in the AIAA Engine Design Competition “Let’s Re-Engine the Concorde” will be used to simulate the Rolls-Royce/SNECMA Olympus 593 and subsequently design a new low bypass ratio turbofan to today’s standards to power the existing Concorde aircraft
LEARNING OBJECTIVES
- To establish the role of performance in an overall gas turbine engine project
- To link design and performance processes
- To convey and relate the roles and interactions of the relevant primary engine components
- To illustrate the application and the power of an easy-to-use performance software to deliver accurate and reliable performance results
- To teach workshop participants to use the software effectively
The workshop is aimed at those who need an engine design and performance tool that is easily used to build models of complete engine to estimate and study performance, such as:
- Engineers in all branches of propulsion research or industry
- Designers of compressors, turbines, and engine systems
- University faculty members who teach courses in propulsion, thermodynamics and aerodynamics and other associated engineering subjects - and their students
- Other propulsion engineering specialists interested in learning about the role of performance in a gas turbine engine program and how to optimize their effectiveness
COURSE FEES (Sign-In To Register)
- AIAA Member Price: $1,395 USD
- Non-Member Price: $1,595 USD
- AIAA Student Member Price: $795 USD
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OUTLINE
1. Basic Principles
1.1 How a Gas Turbine Engine Works
1.2 Engine Configurations
1.3 Major Components
1.4 Nomenclature, Station Numbers, Typical Mach Numbers
1.5 A Simple Turbojet with an Ideal Cycle
1.6 Efficiency & Other Definitions of Performance
2. Turbojets
2.1 A Real Turbojet Cycle
2.2 Augmented Turbojets
2.3 Optimization – A Parametric Study
2.4 Limits
3. Turbofans
3.1 Turbofan Features & Performance Benefits
3.2 Conventional Turbofans: The Quest for Reduced SFC
3.3 Two Spools vs. Three Spools?
3.4 Turbofans with a Gearbox
3.5 Mixed Turbofans
3.6 Augmented Turbofans
3.7 Moving towards High Speed Systems
4. Mechanical Systems
4.1 Introduction
4.2 Flow Path
4.3 “Working Components”
4.4 Frames and Ducts
4.5 Shafts and Bearings
4.6 Disks
4.7 Integration – the Overall Engine
5. Secondary Air Systems
5.1 More than Turbine Cooling …
5.2 … But Mostly Turbine Cooling
6. Compressors
6.1 Function, Environment, Basic Efficiency
6.2 Velocity Diagrams
6.3 Stage Characteristics
6.4 Compressor Design, Blade Flowfield, and Meanline Analysis
6.5 Three-Dimensional Flow & Radial Equilibrium
6.6 Diffusion
6.7 Mean Line Performance & Loss Models
6.8 Some Practical Issues
6 9 Compressor Performance Maps
7. Turbines
7.1 Function, Environment, Basic Efficiency
7.2 Velocity Diagrams
7.3 Stage Characteristics
7.4 Preliminary Design and Analysis
7.5 Mean Line Performance & Loss Models
7.6 Turbine Performance Maps
8. Exhaust Systems
8.1 Simple Convergent Nozzles
8.2 Convergent-Divergent Nozzles
9. Inlets
9.1 Subsonic Inlets
9.2 Mixed Mission Inlets
10. Combustors and Afterburners
10.1 Combustors
10.1.1 Combustor Introduction and Requirements
10.1.2 Combustor Types and Design Considerations
10.1.3 Combustor Efficiency
10.1.4 Combustor Pressure Losses
10.1.5 Combustor Temperature Distribution and Emissions
10.2 Afterburners
10.2.1 Afterburner Components
10.2.2 Afterburner Performance Simulation Requirements
10.2.3 Afterburner Flowfield Characteristics
10.2.4 Afterburner Pressure Losses in Afterburner Operation
10.2.5 Afterburner Efficiency
11. Engine Families
12. Modeling Existing Engines
Summary, Reprise, Questions, Discussion
INSTRUCTOR
Dr. Ian Halliwell obtained his B.Sc. in Aeronautical Engineering and M.Sc. in Aerodynamics from Imperial College, London, followed by a Ph.D. in Experimental Gas Dynamics from the University of Southampton. His professional career began in 1975 at Rolls-Royce, Derby in Turbine Aerodynamics Research. He then crossed the Atlantic to work for Pratt and Whitney Canada in Mississauga and subsequently GE in Cincinnati, where he moved into the preliminary design of complete engine systems and spent a few years on the High Speed Civil Transport program. During that period, he also began teaching in GE after-hours education.
While continuing to model complete engine
systems, his teaching activities continued after moving to the small business
world, as a contractor at the NASA Glenn Research Center and expanded through
involvement with AIAA and ASME/IGTI. He
chaired the AIAA Air Breathing Propulsion and Gas Turbine Engine Technical
Committees and is still an active member of AIAA. He is also a member of the
ASME/IGTI Aircraft Engine and Education Committees. His connection to students and university
faculty was enhanced during the 14 years he organized the AIAA International
Engine Design Competition for undergraduate teams.
Classroom hours / CEUs: 32 classroom hours / 3.2 CEU/PDH
Contact: Please contact Lisa Le or Customer Service if you have questions about the course or group discounts (for 5+ participants).
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