Conceptual Design of an Airfoil with Temperature-Responsive Polymer

Autor: Nejaamtheen, Mohammed Niyasdeen
Jazyk: angličtina
Rok vydání: 2013
Předmět:
DOI: 10.5281/zenodo.1087430
Popis: The accelerated growth in aircraft industries desire effectual schemes, programs, innovative designs of advanced systems and facilities to accomplish the augmenting need for home-free air transportation. In this paper, a contemporary conceptual design of a cambered airfoil has been proposed in order to providing augmented effective lift force relative to the airplane, and to eliminating drawbacks and limitations of an airfoil in a commercial airplane by using a kind of smart materials. This invention of an unsymmetrical airfoil structure utilizes the amplified air momentum around the airfoil and increased camber length to providing improved aircraft performance and assist to enhancing the reliability of the aircraft components. Moreover, this conjectured design helps to reducing airplane weight and total drag.
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Databáze: OpenAIRE
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