1. COMPARISON BETWEEN A400M & A320NEO WHAT IS THE STABILITY ? E.Miraç TERCANLI

2. OUTLINE : 1-WHAT IS THE STABILITY? 2-STABILITY/DYNAMIC OF FLIGHT; A-)STATIK STABILITY ; a-)Pozitive S.S b-)Negative S.S c-)Nötr S.S B-)DINAMIC STABILITY ; a-)Nötr D.S b-)Pozitif D.S c-)Negative D.S 3-)LONGITUDINAL STABILITY 4-)LATERAL STABILITY 5-)DIRECTIONAL STABILITY 6-)AIRBUS A400M ATLAS 7-)AIRBUS A320 NEO 8-)SUMMARY 9-) REFERENCES

3. What is the Stability ? 1-WHAT IS THE STABILITY ?

4. STABILITY AND DYNAMIC OF FLIGHT 2-) STABILITY / DYNAMIC OF FLIGHT A- STATIC STABILITY a- Positive Static Stability b-Negative Static Stability c-Nötr Static Stability B-DYNAMIC STABILITY a-Nötr Dynamic Stability b-Pozitif Dynamic Stability c-Negative Dynamic Stability

5. POSITIVE STATIC STABILITY A- STATIC STABILITY a-Positive Static Stability

6. EQUILIBRIUM POINT NEGATIVE STATIC STABILITY A-STATIC STABILITY b-Negative Stability

7. NOTR STATIC STABILITY A-STATIC STABILITY c-Nötr Static Stability

8. B-DYNAMIC STABILITY Negative Dynamic Stability Positive Dynamic Stability Nötr Dynamic Stability

9. 3-) LONGITUDINAL STABILITY 4-) LATERAL STABILITY

10. Horizontal Axis Vertical Axis Longitudinal Axis Roll Movement Horizontal Stability Linear Stability Yaw Movement Longitudional Stability Pitch Movement 3-)LONGITUDIONAL STABILITY

11. Center of Gravity Horizontal Stability Force of Horizontal Stability Williwaw

12. Center of Gravity Horizontal Stability Force of Stability

13. WIND WING MOVEMENT (TO UPWARD) WING MOVEMENT ( TO DOWNWARD ) 4- LATERAL STABILITY

14. 5-) DIRECTIONAL STABILITY YAW AXIS CENTER OF GRAVITY FIN OR VERTICAL STABILIZER YAW MOVEMENT FLIGHT ROUTE

15. FLIGHT MOVEMENT YAW MOVEMENT LARGE SURFACE AREASMALL SURFACE ALANI

16. AIRBUS A320 NEO : HIGH RESISTANCE/TWISTED BLADE WINGS(SHARKLETS) 2 SMART TURBOFAN ENGINES(LEAP-X) *NARROW BODY /COMPOSITE MATERIAL (ALIMINIUM) LENGHT 37.57M(123FT) *WINGSPAN 34.10M(111 M – FT 101 Ib) BLADE SLOPE 25 *HEIGHT 11.76M(38FT 7in) CABIN WIDTH 3.70 M *BODY WIIDTH 3.95 *EMPTY WEIGHT 42.400 KG-77.000KG * FUEL CAPACITY 29.680 LT

17. AIRBUS A400M ATLAS : *CARBON FIBRE REINFORCED PLASTIC *LENGHT 45.1 M *WINGSPAN 42.4M *HEIGHT 114.7M *WING AREA 225.1 M2 *EMPTY WEIGHT 76.500KG *GROSS WEIGHT 120.000KG *MAX TAKEOFF WEIGHT 141.000KG *FUEL CAPACITY 50.500 KG *MAX LANDING WEIGHT 122.000KG POWERPLANT 4 X EUROPROP TP400-D6 PROPELLERS 8 BLADED https://www.youtube.com/watch?v=fRtOGJT qjkQ https://www.youtube.com/watch?v=fRtOGJT qjkQ

19. REFERENCES : http://www.allstar.fiu.edu.tr http://www.megep.meb.gov.tr http://en.wikipedia.org www.youtube.com

20. PLT 104/B ÇAGLAR ÜÇLER(LECTURER) 02/03/2015 Prepared by EYYUP MIRAC TERCANLI