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Flight profiles, engine thrusts and aeroplane flight speeds might be supplied# Q N. s; ^1 _3 a/ [
directly for an aeroplane type undergoing reference flight procedures (see 4.2.2). Then, for
0 t. J; e7 O% A6 M! u8 t5 m2 B# i8 zoperations at an airport where the actual procedures in use are unknown, these reference D: L1 s! m/ V# A- s. l, z
procedures can be assumed. The information for other procedures known to be used, or for, P! l$ ^) p; O/ U& R( p9 I* F: _% l
different operating conditions of the aeroplane, can be calculated using aerodynamic and thrust* C+ H, g& Y. _; [ p) M k+ j+ O) p0 Z
equations. |
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