| 1. | |
PROCESS OF AIRCRAFT DESIGN | - CONCEPTUAL DESIGN PHASE - PRELIMINARY DESIGN PHASE - PRODUCTION(DETAIL) DESIGN PHASE |  |
| 2. | |
OVERVIEW 1 | - REGULATIONS AND SPECIFICATIONS - Certification & Airworthiness | |
| 3. | |
OVERVIEW 2 | - STRUCTURE DESIGN CYCLE - LOAD FACTOR COMPARISON | |
| 4. | |
DESIGN GUIDELINES | - COMMERCIAL TRANSPORT PRICE COMPARISON - GROUND RULES OF A SUCCESSFUL AIRFRAME ENGINEER - AIRFRAME POST-DESIGN RELATIONSHIP | |
| 5. | |
BASIC LOADS | - AIRCRAFT LOADS - LANDING GEAR LOADS - MISCELLANEOUS LOADS | |
| 6. | |
MATERIAL SELECTION 1 | - MATERIAL SELECTION CRITERIA - ALUMINUM ALLOYS | |
| 7. | |
MATERIAL SELECTION 2 | - TITANIUM ALLOYS - STEEL ALLOYS | |
| 8. | |
Mid-term exam. | |
|
| 9. | |
WING STRUCTURE 1 | - WING BOX STRUCTURAL ARRANGEMENT - WING COVERS - SKIN-STRINGER PANEL DESIGN | |
| 10. | |
WING STRUCTURE 2 | - WING SPARS - WING RIBS | |
| 11. | |
WING STRUCTURE 3 | - WING ROOT JOINTS - WING CARRY-THROUGH STRUCTURES - WING PYLON MOUNT - MAIN LANDING GEAR SUPPORT | |
| 12. | |
EMPENNAGE DESIGN | - DESIGN REQUIREMENTS - HORIZONTAL STABILIZER STRUCTURES - ROOT JOINTS | |
| 13. | |
COMPOSITE LAMINATE DESIGN 1 | - APPLICATION OF COMPOSITES TO AIRCRAFT - COMPOSITE DESIGN CONSIDERATION - COMPOSITE ANISOTROPY | |
| 14. | |
COMPOSITE LAMINATE DESIGN 2 | - GENEALCOMPOSITES FOR TAPE LAY-UP LAMINATE - DELAMINATION - PAD-UP AND PLY DROP-OFF - THERMAL EXPANSION EFFECTS | |
| 15. | |
COMPOSITE LAMINATE DESIGN 3 | - FATIGUE AND DAMAGE - HYBRIDS - DESIGN ALLOWABLE - SKIN-STRINGER PANEL DESIGN | |
대구광역시 동구 동내로 64(동내동 1119) 우)41061
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