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Flight profiles, engine thrusts and aeroplane flight speeds might be supplied
, ]5 W& k$ s9 q5 K) h1 e T. hdirectly for an aeroplane type undergoing reference flight procedures (see 4.2.2). Then, for
8 @4 s, l- P) {operations at an airport where the actual procedures in use are unknown, these reference
. c/ h" K% A& fprocedures can be assumed. The information for other procedures known to be used, or for- A! R7 K( t, m, U+ B ?
different operating conditions of the aeroplane, can be calculated using aerodynamic and thrust6 o. n+ `% a: {% u6 a+ b: m. \! t# u
equations. |
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