Stress. Weight. Wing
http://ninova.itu.edu.tr/tr/dersler/ucak-uzay-
fakultesi/1005/uck-451e/. TEXTBOOK: Aircraft Design: A Conceptual Approach.
TEXTBOOK: Aircraft Design: A Conceptual Approach Raymer D. P, 2006,, Fourth Edition, AIAA Education Series, New York, NY, ISBN:1-56347-829
Fuselage
Hydrolics
Loft
Powerplant
Production
OTHER REFERENCE: Airplane Design
Aerodynamics
Armanent
Electrical
Empennage
[email protected]
Control
Equipment
Service
Wing
Stress
Weight
Roskam J., 2003,, parts: 1-8, Design, Analysis and Research (DAR) Corporation, ISBN:1-884885-42 2
http://ninova.itu.edu.tr/tr/dersler/ucak-uzay-fakultesi/1005/uck-451e/
Weeks 1 2 3 4 5 6 7 8 9 10 11 12 13 14
Topics Introduction Project Definition Competitor Study First Guess Sizing Airfoil and Geometry Selection Thrust to Weight Ratio and Wing Loading Midterm Examination Initial Sizing Configuration Layout and Loft Configuration Layout and Loft Propulsion and Fuel System Integration Landing Gear and Subsystems Aerodynamics Aerodynamics
1. Introduction to Aircraft Design Phases of aircraft design, aircraft conceptual design process, takeoff weight buildup, empty weight estimation, fuel-fraction estimation, takeoff-weight calculation
2. Airfoil and Geometry Selection Airfoil selection, wing geometry, tail geometry and arrangement
3. Thrust to Weight Ratio and Wing Loading Thrust to weight ratio, wing loading, selection of thrust to weight and wing loading
4. Initial Sizing Rubber engine sizing, fixed engine sizing, geometry sizing, control surface sizing
5. Configuration Layout and Loft End products of configuration layout, conic lofting, conic fuselage development, flat-wrap fuselage lofting, circle to square adapter, fuselage loft verification, wing tail layout and loft, aircraft layout procedures, wetted area determination, volume determination, special considerations
6. Propulsion and Fuel System Integration Propulsion selection, jet-engine performance and integration, propeller-engine performance and integration, fuel system
7. Landing Gear and Subsystems Landing gear arrangements, tire sizing, shock absorbers, castoring wheel geometry, gear retraction geometry, seaplanes, subsystems
8. Aerodynamics Aerodynamic forces, Lift, Parasite drag, Induced drag, CFD
Activities Midterm Exams
Quantity Effects on Grading, % 1
20
Projects
9
20
Term Paper/Project
1
15
1
40
Quizzes Homework
Laboratory Work Other Activities Final Exam
5