High performance aircraft are, by their very nature, often required to undergo manoeuvres involving high angles of attack. Under these conditions unsteady vortices emanating from the wing and the fuselage will impinge on the twin fins (required for directional stability) causing excessive buffet loads, in some circumstances, to be applied to the aircraft. These loads result in oscillatory stres...

Due to the dynamic development of environmentally friendly aircraft propulsion, paper describes effect distributed propulsion on emission and fuel consumption changes in comparison with traditional propulsion. A is a composed set units located leading edges wings or fuselage, generating thrust symmetrically both sides fuselage. The analysis was based technical data AOS H2 motor glider. During t...

Abstract In this study, the jig-less end-effector system developed to assemble components of a full-scale multifunctional integrated composite thermoplastic lower fuselage section is tested and validated. To offset environmental impact higher volume air transport, aviation industry wants design lighter more environmentally friendly aircraft. achieve this, there need exploit novel materials tech...