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Dynamics of Aircraft Flight (Hardcover)
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Dynamics of Aircraft Flight (Hardcover)
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Performance calculations can be classified into three main types:
lift, thrust and slope. Firstly, since the lift profile is known
and unmodifiable from the time an aircraft is designed, the mass at
a given speed or the speed at a given mass must be determined.
Then, once the thrust of the engines and the mass are known, the
slope must be calculated. Finally, once the slope is known (for
example, level flight) as well as the mass, it is necessary to
deduce the thrust; this is the position of the throttle control
lever that ensures balance. The corresponding consumption must then
be defined. Performance specifications for customer aircraft, such
as manoeuvrability, fuel consumption, maintenance, safety and
testability, have become ever more demanding with each generation
of equipment. Major technical advances have been required: wing
profiles, engines, materials to reduce mass, etc. This book
presents a theoretical approach to flight mechanics that makes it
possible to grasp the subject and links it with the empirical
approach of manufacturers.
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