Results 11 to 20 of about 35,333 (231)
The hybrid Ice Protection System combining thermoelectric and superhydrophobic coating is efficient and benefits from low-energy consumption. In order to explore the application details of superhydrophobic coating, this paper investigated the ...
Lei Yu, Yuan Wu, Huanyu Zhao, Dongyu Zhu
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Modeling high-dimensional aerodynamic data presents a significant challenge in aero-loads prediction, aerodynamic shape optimization, flight control, and simulation.
Bo-Wen Zan +4 more
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Study on Aerodynamic Interference of Tanker Aircraft on Receiver Aircraft based on N-S Equations
The wake flow field of tanker aircraft can produce the complex flow interference on receiver aircraft during aerial refueling.The computational fluid dynamics(CFD)method based on Navier-Stokes(N-S)equations is used to analyze the wake flow field of the ...
GENG Yansheng +3 more
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Experimental investigation on effect of partial flexibility at low aspect ratio airfoil – Part I: Installation on suction surface [PDF]
Effects of flexible membrane mounted over suction surface of NACA 4412 airfoil were experimentally investigated at Reynolds number of 5x104 and low aspect ratio (AR=1) in this paper.
Genç Mustafa Serdar +2 more
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The effect of the Reynolds number on the flying wing common research model with a large sweep angle and small aspect ratio is studied by numerical simulation.
Peng Lin +9 more
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Cognition and Discussion on New Thermal Barrier of Hypersonic Vehicles
In the future, high-speed vehicles will develop towards the integration of aviation and aerospace technologies, such as longer range and faster speed, and constantly break through the boundary of flight speed and cruising space.
Bang-cheng AI +7 more
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Analysis of Development Trend and Design Technology of Hard Type Air Tanker
Air refueling technology reflects the strength of a country's air force to a certain extent, and has been widely concerned. The development history of hard type air tanker is summarized in this paper.
WANG Xiuxiang, GAO Xu, GAO Yakui
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Most existing aerodynamic shape optimization (ASO) studies do not take the balanced pitching moment into account and thus the optimized configuration has to be trimmed to ensure zero pitching moment, which causes additional drag and reduces the benefit ...
Kai Wang +3 more
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With the aim for a low-aspect-ratio flying wing configuration, this study explores the influence of wall temperature gradient on the laminar and turbulent boundary layers of aircraft surface and determines the effect on the transition Reynolds number and
Peng Lin +6 more
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A High Efficient Fluid-Structure Interaction Method for Flutter Analysis of Mistuned [PDF]
The time cost is very high by direct fluid-structure interaction method for mistuned bladed disk structures, so aerodynamic loads generally are ignored or treated as small perturbations in traditional flutter analysis.
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