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Flight profiles, engine thrusts and aeroplane flight speeds might be supplied
4 W+ C, Y) e- A/ p8 w, Idirectly for an aeroplane type undergoing reference flight procedures (see 4.2.2). Then, for7 w0 ^6 i; k/ n" }( T& A/ k
operations at an airport where the actual procedures in use are unknown, these reference' n# @4 T' h, x1 {" n W
procedures can be assumed. The information for other procedures known to be used, or for
; n. R$ s- k/ ], V J" C- adifferent operating conditions of the aeroplane, can be calculated using aerodynamic and thrust, d2 G. O8 O2 ~5 K. B' x# a) Y1 J+ f
equations. |
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