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Fuzzy logic based nonlinear blending hybrid control of a kestrel-inspired ornithopter operating in sinusoidal and dryden gusts. [PDF]
Abbasi SH +3 more
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A three-level discretization framework for dynamic behaviors of graphene-coated rotational blades with preset-angle sandwich structure under complex loads. [PDF]
Bai B +7 more
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The Structural Design and Optimization of a Novel Independently Driven Bionic Ornithopter. [PDF]
Dai M +6 more
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Optimized super-twisting active disturbance rejection control based on nonlinear extended state observer for aircraft attitude stabilization. [PDF]
Yazdiniya F, Ansarifar G.
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Structural optimization using computational aerodynamics
AIAA Journal, 2000A recently developed methodology for aircraft structural design, based on nonlinear airloads, is extended to include a modal-based optimization option and is employed with a new computational aerodynamics code for loads analysis. Nonlinear maneuver loads are evaluated by a computational scheme that efficiently combines fluid dynamics iterations with ...
Daniella E. Raveh +2 more
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Aerodynamic optimization using proficient optimization algorithms
2012 International Conference on Computing, Communication and Applications, 2012Nowadays engineering analysis relies heavily on computer-based solution algorithms to investigate the performance of an engineering system. Computational fluid dynamics (CFD) is one of the computer-based solution methods which are more widely employed in aerospace engineering.
R. Mukesh, K. Lingadurai, S. Karthick
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Aerodynamic design via optimization
Journal of Aircraft, 1992An aerodynamic design optimization method is presented that generates an airfoil, producing a specified surface pressure distribution at a transonic speed. The design procedure is based on the coupled Euler and boundary-layer technology to include the rotational viscous physics which characterizes transonic flows.
K. D. Lee, S. Eyi
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Aerodynamic optimization of cyclorotors
Aircraft Engineering and Aerospace Technology, 2016Purpose Cycloidal rotors, also known as cyclogyros, are horizontal axis rotary-wing machines with potential for Vertical Take-Off and Landing aircraft applications. The paper aims to devise and validate a new semi-empirical analytical model that is capable of assisting in the structural and aerodynamic design of cyclogyros.
Jakson Augusto Leger Monteiro +2 more
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