In early stages of an aircraft design process, it is necessary to
determine the minimum thrust or power requirement and rapidly
select the appropriate propulsion, which involves a tight coupling
between flight performance and missions' analyses, engine
performance prediction and design optimisation. The first chapter
of this book provides an overview of how to determine the minimum
thrust or power requirements for jet and propeller driver transport
aircraft. The second chapter examines the comprehensive modeling
and design of production processes of aircraft assembly. The final
chapter focuses on the computational modeling of the Be-200 and
Be-103 amphibious aircraft models.
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