%0 Thesis
%A Calle Merchán, Carlos de la
%8 2024-06
%U https://hdl.handle.net/20.500.12880/8415
%X The fact of substituting the horizontal stabilizer of an aircraft appeared since the necessity of
aviation to lower the weight of aircraft in order to generate fewer emissions as well as allowing
the airlines to offer even cheaper flights so that to achieve a better accessibility to the aerospace
sector for a bigger percentage of the population. This study will carry out not only the re-design
of aircraft’s tail but also, CFD (Computational Fluid Dynamics) analysis would be performed to
see if this new configuration could be or not possible by the calculation of different performance
parameters. Because of the climatological situation of the world, reducing the emissions and so
making flights as efficient as possible constitute some of the key parameters to consider for the
future of aircraft design; due to this, the design of this system was also performed considering
these factors meticulously in addition to the investigation about the introduction of propfan engines
to substitute the conventional jet engines.
%T Lifting System Replacement For A Horizontal Stabilizer
%K Estabilizador horizontal
%K Motores propfan
%K Emisiones
%~ END