<p>AEEM 519 and 523 Engine Design I & II Catalog data: 20-AEEM-519/523. Engine Design I & II 4 cr. ea & 8 cr. total. 519: Integrated propulsion/vehicle system performance, mission/constraints. Trade off studies design and off design cycle analysis and optimization. 523: Engine flow path and sizing. Intake, turbomachinery, combustor and exhaust system design. Report preparation and formal presentation Prerequisites: 20-AEEM-382 Aerospace Vehicle Performance; 20-AEEM-445 Gas Dynamics; 20-AEEM- 474 Airbreathing Propulsion Textbook: Aircraft Engine Design, J.D. Mattingley, W.H. Heiser, and D.H. Daley, AIAA, New York, New York, 2002: 1563475383 Coordinator: Awatef Hamed, Professor of Aerospace Engineering & Engineering Mechanics, 745E Baldwin, 556-3553 [email protected]</p><p>Check corresponding rating block Rate how well the objectives are being met Course Objectives (5 = highest, 1 = lowest)</p><p>The students will be able to: 5 4 3 2 1</p><p>1. Construct an aircraft constraint diagram from requirements given in an RFP [a, b, c, e, k] 2. Calculate the fuel required for a given mission using engine performance estimates [a, b, e, k] 3. Use an engine code to select the best design point parameters [c, e, k] 4. Use an engine code to calculate off-design performance [e, k] 5. Select an engine design point for a given mission and size the engine [b, c, e, h, j] 6. Define global and interface quantities required for the component design teams [c, d] 7. Outline design methods for all engine components [a, b, c] 8. Design engine components [c, k]</p><p>9. Experience participation in a design team effort [d] 10. Make a professional presentation as a team to a panel of engineers from industry [g, h, j] 11. Prepare a well-documented team report of the design methodology and trade-off studies [d, g, h, i] Comments (use reverse if necessary):</p>