Publicado 6 números por año
ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604
OPTIMAL DESIGN OF THE NACELLE ASSEMBLY UNDER THE WING OF AN AIRLINER BASED ON RANS NUMERICAL SIMULATIONS
SINOPSIS
The key elements of the methodology of using the results of numerical simulations for the optimal aerodynamic design loop implemented in a basic propulsion system nacelle assembly under the wing of an airliner are considered. To illustrate the potentials of the considered methodology, the results of the optimization of the pylon geometry and spatial location of a high-bypass-ratio engine nacelle placed under the wing of a midrange airliner are presented.
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