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

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Presentation transcript:

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

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

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

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

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

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

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

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

3-) LONGITUDINAL STABILITY 4-) LATERAL STABILITY

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

Center of Gravity Horizontal Stability Force of Horizontal Stability Williwaw

Center of Gravity Horizontal Stability Force of Stability

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

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

FLIGHT MOVEMENT YAW MOVEMENT LARGE SURFACE AREASMALL SURFACE ALANI

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 KG KG * FUEL CAPACITY LT

AIRBUS A400M ATLAS : *CARBON FIBRE REINFORCED PLASTIC *LENGHT 45.1 M *WINGSPAN 42.4M *HEIGHT 114.7M *WING AREA M2 *EMPTY WEIGHT KG *GROSS WEIGHT KG *MAX TAKEOFF WEIGHT KG *FUEL CAPACITY KG *MAX LANDING WEIGHT KG POWERPLANT 4 X EUROPROP TP400-D6 PROPELLERS 8 BLADED qjkQ qjkQ

REFERENCES :

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