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Extra resources for Aviation Weather Surveillance Systems - Advanced Radar and Surface Sensors for Flight Safety and Air Traffic Management
2 Typical dependence of lift coefficient of an aerofoil on the angle of attack 1 The term 'undisturbed' is used here in the context of the disturbance to the air caused by the flight of the aircraft itself, and does not pertain to the disturbances due to weather and other factors. An aircraft in flight would create a flow field around itself and thus affect the state of the air in its own vicinity relative to the undisturbed air far away. g. 3 b The smooth, streamlined flow of air past an aerofoil at low angle of attack (a), and separated flow accompanied by turbulence at high angles of attack (b) said to be stalling.
The purpose here is, however, not to cover all aspects of aviation, but essentially those which may have a bearing on the focus of this book. 2 Phases of aircraft flight The sequence of stages through which the flight of an aircraft passes, starting from parking at the origin, consists of taxiing, takeoff, climb, cruise, descent, landing and taxiing, before again parking at the destination. The flight environment and parameters are different in each of these stages, and the nature of weather phenomena varies with altitude.
A necessary condition for normal flight of an aircraft is its dynamic stability which ensures that oscillations, once induced, die down on their own, though the damping process may be further aided by programmed control action on the part of the pilot or autopilot. Two velocity parameters are of great importance in describing the motion of an aircraft. The ground speed of the aircraft refers to its speed (or, more generally, its velocity) relative to the ground underneath. This speed parameter is important for determining the aircraft's motion between fixed points on the earth.