IMPROVEMENT OF OPERATIONAL CHARACTERISTICS OF THE AIRCRAFT WITH A DEFORMABLE COMBINED WING
Journal Title: Інформаційні системи, механіка та керування - Year 2015, Vol 0, Issue 12
Abstract
of performance of flying machines with different types of bearing surfaces with equal specific wing loading G / S. Development of experimental aircrafts with soft wings due to the need to increase the operation of aircrafts. The results of wind tunnel test has performed using a general purpose classical scheme for models plane (Aeroprakt A-20) and are provided with two different types of wing skin: completely rigid wing and hybrid wing, which consists of 30% hard part and 70% soft inflatable portion. By correction of wind tunnel test results Aeroprakt aircraft A-20, derived from the characteristics of the deformable wing aircraft. Based on the research performance of experimental and computational models of the comparative analysis of aircraft performance characteristics of the aircraft with the wing skin of different types at equal specific wing loading G / S. The above article results demonstrate the possibility of using a general-purpose design of the proposed design solution aircraft - carrying surface, the combination of a rigid front and rear inflatable parts.
Authors and Affiliations
Dmytro Zinchenko,, Gurkan Ortamevzi
Keywords
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