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COMPARISON BETWEEN A400M & A320NEO WHAT IS THE STABILITY ? E.Miraç TERCANLI
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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
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What is the Stability ? 1-WHAT IS THE STABILITY ?
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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
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POSITIVE STATIC STABILITY A- STATIC STABILITY a-Positive Static Stability
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EQUILIBRIUM POINT NEGATIVE STATIC STABILITY A-STATIC STABILITY b-Negative Stability
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NOTR STATIC STABILITY A-STATIC STABILITY c-Nötr Static Stability
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B-DYNAMIC STABILITY Negative Dynamic Stability Positive Dynamic Stability Nötr Dynamic Stability
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3-) LONGITUDINAL STABILITY 4-) LATERAL STABILITY
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Horizontal Axis Vertical Axis Longitudinal Axis Roll Movement Horizontal Stability Linear Stability Yaw Movement Longitudional Stability Pitch Movement 3-)LONGITUDIONAL STABILITY
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Center of Gravity Horizontal Stability Force of Horizontal Stability Williwaw
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Center of Gravity Horizontal Stability Force of Stability
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WIND WING MOVEMENT (TO UPWARD) WING MOVEMENT ( TO DOWNWARD ) 4- LATERAL STABILITY
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5-) DIRECTIONAL STABILITY YAW AXIS CENTER OF GRAVITY FIN OR VERTICAL STABILIZER YAW MOVEMENT FLIGHT ROUTE
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FLIGHT MOVEMENT YAW MOVEMENT LARGE SURFACE AREASMALL SURFACE ALANI
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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
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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
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REFERENCES : http://www.allstar.fiu.edu.tr http://www.megep.meb.gov.tr http://en.wikipedia.org www.youtube.com
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PLT 104/B ÇAGLAR ÜÇLER(LECTURER) 02/03/2015 Prepared by EYYUP MIRAC TERCANLI
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