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Improvement of aerodynamic performance of supersonic aircraft using canard surface with TVFC. (English) Zbl 1179.93134

Summary: The purpose of increasing the aerodynamic efficiency and enhancing the supermaneuverability for the selected supersonic aircraft is presented. Aerodynamic characteristics, the surface pressure distribution and the maximum lift are estimated for the baseline configuration for different Mach numbers and attack angles in subsonic and supersonic potential flows, using a low-order three-dimensional panel method supported with the semi-empirical formulas of the data compendium (DATCOM). Total nose-up and nose-down pitching moments about the center of gravity of the complete aircraft in the subsonic region depending on flight conditions and aircraft performance limitations are estimated. A software package is developed to implement the two-dimensional thrust vectoring flight control technique (pitch vectoring up and down) controlled by the advanced aerodynamic and control surface (the foreplane or the canard). Results show that the canard with the thrust vectoring produces enough nose-down moment and can support the stabilizer at high maneuvers. The suggested surface can increase the aerodynamic efficiency (lift-to-drag ratio) of the baseline configuration by \(5\%-6\%\) in subsonic and supersonic flight regimes.

MSC:

93C95 Application models in control theory
93C20 Control/observation systems governed by partial differential equations
93B18 Linearizations
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