Take-off and landing of aicraft
Journal Title: INCAS BULLETIN - Year 2012, Vol 4, Issue 2
Abstract
In this paper, the take-off and landing segments of an airplane trajectory are studied. The equations of motion for the ground run are derived and solved for distance. Then, specific formulas are obtained for the take-off ground distance and time and the landing ground distance and time. Transitions from take-off to climb and descent to landing are investigated so that take-off distance and landing distance and time can be estimated. The run distances and the run times for take-of and landing dependent of altitude, speed wing, temperature, the coefficient of rolling friction. In conformity with mathematical model, programs of calculation were elaborated. Also interfaces of calculations were elaborated for programs of calculation.
Authors and Affiliations
Vasile ISTRATIE, Nicolae APOSTOLESCU
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