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Week - 1 |
aerodynamic design: airfoil, wing parameters, fuselage and wing configurations, control surfaces, performance and stability analysis |
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Week - 2 |
structural design: material, strength analysis and testing, wing and fuselage construction; |
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Week - 3 |
propulsion : engine, propeller, performance analysis and testing |
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Week - 4 |
Avionics and Control; control parameters, control units and integration; |
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Week - 5 |
optimization of all parameters according to the Project requirements and integration |
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Week - 6 |
manufacturing: prototype and flight testing; Project presentation and reporting. |
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Week - 7 |
Project presentation and reporting rules |
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Week - 8 |
Designed Airplane; Whole aircraft lift, whole aircraft drag, Drag polar |
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Week - 9 |
Performance of the Designed Aircraft; Equations of motion, Propulsion, Drag Curves, lift to drag ratio, power curves |
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Week - 10 |
Performance of the Designed Aircraft;; Gliding, Climbing, Range and Endurance, Landing and Takeoff, Turns, V-n diagrams |
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Week - 11 |
Stability and Control of the Designed Aircraft;; Longitudinal Control Analysis, Longitudinal Stability, Dynamic Longitudinal Stability |
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Week - 12 |
Stability and Control of the Designed Aircraft;; Longitudinal Control Analysis, Longitudinal Stability, Dynamic Longitudinal Stability |
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Week - 13 |
Stability and Control of the Designed Aircraft; Lateral and Directional Stability, Dynamic Stability and Control, Lateral and Directional Stability |
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Week - 14 |
Presentations of the Detailed Reports |
Eskisehir Technical University Info Package