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时间:2011-11-26 15:59来源:蓝天飞行翻译 作者:航空

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TOGA  Take-Off/Go-Around 
TOGW  Take-Off Gross Weight 
TOR  Take-off Run 
TOW  Take-Off Weight 
UTC  Coordinated Universal Time 
V1  Critical engine failure speed 
V2  T/O safety speed 
VAPP  Final approach speed 
VFR  Visual Flight Rules 
VHF  Very High Frequency (30 - 300 
MHz) 
VLS  Lowest selectable speed 
VMC  Minimum control speed 
VMU  Minimum unstick speed 
VOR  VHF Omnidirectional Range 
VR  Rotation speed 

VREF  Landing reference speed 
VS  Stalling speed (=VS1g for 
Airbus FBW aircraft) 
WAI  Wing Anti Ice 
WPT  Waypoint 
WX  Weather 
WXR  Weather Radar 

ZFW Zero Fuel Weight

26


A. AIRCRAFT CONTAMINATION IN FLIGHT

The objective of this chapter is to explain some of the difficulties encountered by flight crews in winter time or cold/wet air. Many forms of ice may deposit or accrete on the airframe, in flight or on ground, and that will affect aircraft performance. It is difficult to determine how much the performance is affected. There are cases when the amount of ice looks benign and proves to produce large performance degradation. The opposite case may also be true.
However, thorough analysis of the incident/accident record strongly suggests that enhanced pilot awareness of icing is a key factor in dominating the icing threat.
A1 ICING PRINCIPLES
A1.1 Atmospheric physics at a glance
Water is a well-known component of atmospheric air. Clear air includes water vapor in very variable proportions according to air temperature (SAT or OAT). The maximum amount of water vapor allowable in the air is about 0.5 g/m3 at - 30°C and 5 g/m3 at 0°C for moderate altitudes. These limiting conditions are called saturation.
Any amount of water in excess of the saturation conditions will show under the form of water drops or ice crystals. These form clouds.
Saturation conditions may be exceeded by two processes:
-First, is the lifting of warm air. Air lifting may be produced by meteorological instability or orography. Instability is associated with weather systems, perturbations or large amounts of clouds. Orographic effect is due to wind blowing onto a mountain, hence lifting on the exposed side.
- Second is the rapid cooling of the lower air layer during a night with clear sky.
In both of these conditions, the amount of water initially present in the air mass may become in excess of the saturation conditions at the new (lower) temperature. Excess water precipitates in the form of drops, droplets or ice crystals.
The icing phenomenon is due to the fact that water does not necessarily turn into ice just at, or below 0°C. Water at negative Celsius temperature may remain liquid; then, it is called supercooled. But supercooled drops and droplets are unstable. This means that they can freeze all of a sudden if they hit, or are hit by, an object, especially if the object is at negative temperature. That is the basic mechanism for aircraft icing.
 
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