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Flight profiles, engine thrusts and aeroplane flight speeds might be supplied) s2 f4 ?, E: B; O
directly for an aeroplane type undergoing reference flight procedures (see 4.2.2). Then, for
/ I% Z4 a6 p* U& joperations at an airport where the actual procedures in use are unknown, these reference. w8 O2 L# T* b
procedures can be assumed. The information for other procedures known to be used, or for7 O9 ~/ R X# ^# u+ {5 ?, y
different operating conditions of the aeroplane, can be calculated using aerodynamic and thrust
( _+ ]" N" M9 }, ^) a0 C, |- J" d) lequations. |
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