時(shí)間：2017-11-06 16:55來(lái)源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點(diǎn)擊：次
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Getting to Grips with Aircraft Performance TABLE OF CONTENTS
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TABLE OF CONTENTS
1. INTRODUCTION
A. GENERAL
1. THE INTERNATIONAL STANDARD ATMOSPHERE (ISA)
1.1. STANDARD ATMOSPHERE MODELING
1.1.1. TEMPERATURE MODELING
1.1.2. PRESSURE MODELING
1.1.3. DENSITY MODELING
1.2. INTERNATIONAL STANDARD ATMOSPHERE (ISA) TABLE
2. ALTIMETRY PRINCIPLES
2.1. GENERAL
2.2. DEFINITIONS
2.3. EFFECTS OF ALTIMETER SETTING AND TEMPERATURE
2.3.1. ALTIMETER SETTING CORRECTION
2.3.2. TEMPERATURE CORRECTION
3. OPERATING SPEEDS
3.1. CALIBRATED AIR SPEED (CAS)
3.2. INDICATED AIR SPEED (IAS)
3.3. TRUE AIR SPEED (TAS)
3.4. GROUND SPEED (GS)
3.5. MACH NUMBER
3.6. TRUE AIR SPEED (TAS) VARIATIONS
4. FLIGHT MECHANICS
B. AIRCRAFT LIMITATIONS
1. FLIGHT LIMITATIONS
1.1. LIMIT LOAD FACTORS
1.2. MAXIMUM SPEEDS
1.3. MINIMUM SPEEDS
1.3.1. MINIMUM CONTROL SPEED ON THE GROUND: VMCG
1.3.2. MINIMUM CONTROL SPEED IN THE AIR: VMCA
1.3.3. MINIMUM CONTROL SPEED DURING APPROACH AND LANDING: VMCL
1.3.4. MINIMUM UNSTICK SPEED: VMU
1.3.5. STALL SPEED
2. MAXIMUM STRUCTURAL WEIGHTS
2.1. AIRCRAFT WEIGHT DEFINITIONS
2.2. MAXIMUM STRUCTURAL TAKEOFF WEIGHT (MTOW)
2.3. MAXIMUM STRUCTURAL LANDING WEIGHT (MLW)
2.4. MAXIMUM STRUCTURAL ZERO FUEL WEIGHT (MZFW)
2.5. MAXIMUM STRUCTURAL TAXI WEIGHT (MTW)
3. MINIMUM STRUCTURAL WEIGHT
4. ENVIRONMENTAL ENVELOPE
TABLE OF CONTENTS Getting to Grips with Aircraft Performance
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5. ENGINE LIMITATIONS
5.1. THRUST SETTING AND EGT LIMITATIONS
5.2. TAKEOFF THRUST LIMITATIONS
C. TAKEOFF
1. INTRODUCTION
2. TAKEOFF SPEEDS
2.1. OPERATIONAL TAKEOFF SPEEDS
2.1.1. ENGINE FAILURE SPEED: VEF
2.1.2. DECISION SPEED: V1
2.1.3. ROTATION SPEED: VR
2.1.4. LIFT-OFF SPEED: VLOF
2.1.5. TAKEOFF CLIMB SPEED: V2
2.2. TAKEOFF SPEED LIMITS
2.2.1. MAXIMUM BRAKE ENERGY SPEED: VMBE
2.2.2. MAXIMUM TIRE SPEED: VTIRE
2.3. SPEED SUMMARY
3. RUNWAY LIMITATIONS
3.1. TAKEOFF DISTANCES
3.1.1. REGULATORY BACKGROUND
3.1.2. TAKEOFF DISTANCE (TOD)
3.1.3. TAKEOFF RUN (TOR)
3.1.4. ACCELERATE-STOP DISTANCE (ASD)
3.1.5. INFLUENCE OF V1 ON ACCELERATE-GO/STOP DISTANCES
3.2. AVAILABLE TAKEOFF LENGTHS
3.2.1. TAKEOFF RUN AVAILABLE (TORA)
3.2.2. TAKEOFF DISTANCE AVAILABLE (TODA)
3.2.3. ACCELERATE-STOP DISTANCE AVAILABLE (ASDA)
3.2.4. LOSS OF RUNWAY LENGTH DUE TO ALIGNMENT
3.2.5. INFLUENCE OF V1 ON THE RUNWAY-LIMITED TAKEOFF WEIGHT
4. CLIMB AND OBSTACLE LIMITATIONS
4.1. TAKEOFF FLIGHT PATH
4.1.1. DEFINITIONS
4.1.2. TAKEOFF SEGMENTS AND CLIMB REQUIREMENTS
4.1.3. MINIMUM AND MAXIMUM ACCELERATION HEIGHTS
4.1.4. TAKEOFF TURN PROCEDURE
4.2. OBSTACLE CLEARANCE
4.2.1. GROSS AND NET TAKEOFF FLIGHT PATHS
4.2.2. OBSTACLE CLEARANCE DURING A STRAIGHT TAKEOFF
4.2.3. OBSTACLE CLEARANCE DURING A TURN
4.2.4. LOSS OF GRADIENT DURING A TURN
4.2.5. TAKEOFF FLIGHT PATH WITH OBSTACLES
4.2.6. TAKEOFF FUNNEL
5. OUTSIDE ELEMENTS
5.1. WIND
5.2. PRESSURE ALTITUDE
5.2.1. EFFECT ON AERODYNAMICS
5.2.2. EFFECT ON ENGINES
5.2.3. SUMMARY
Getting to Grips with Aircraft Performance TABLE OF CONTENTS
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5.3. TEMPERATURE
5.3.1. EFFECT ON AERODYNAMICS
5.3.2. EFFECT ON ENGINES
5.3.3. SUMMARY
5.4. RUNWAY SLOPE
5.5. RUNWAY CONDITIONS (DRY, DAMP, WET, CONTAMINATED)
5.5.1. DEFINITIONS
5.5.2. EFFECT ON PERFORMANCE
5.5.3. AIRCRAFT MANUFACTURER DATA
5.5.4. TAKEOFF PERFORMANCE ON WET AND CONTAMINATED RUNWAYS
6. MAXIMUM TAKEOFF WEIGHT DETERMINATION
6.1. SPEED OPTIMIZATION PROCESS
6.2. REGULATORY TAKEOFF WEIGHT CHART (RTOW CHART)
7. FLEXIBLE AND DERATED TAKEOFF
7.1. FLEXIBLE TAKEOFF
7.1.1. DEFINITION
7.1.2. FLEXIBLE TAKEOFF AND RUNWAY STATE
7.1.3. FLEXIBLE TEMPERATURE DETERMINATION
7.1.4. FLEXIBLE TAKEOFF PROCEDURE
7.2. DERATED TAKEOFF
7.2.1. DEFINITION
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