Aerodynamic Characteristics of a Tandem Flapping Wing in Inclined Stroke Plane Hovering with Ground Effect. [PDF]
Biomimetics (Basel)Shanmugam AR, Sohn CH, Park KS.
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Photochromism‐Driven Full Solar Spectrum Absorption for Efficient Photo‐Thermo‐Electric Conversion
Advanced Science, EarlyView.After electron‐transfer photochromism, a black viologen‐based organic compound shows full solar spectrum absorption (250–2500 nm) and near‐infrared photothermal conversion efficiency (NIR‐PCE) >60%. Integrated with a thermoelectric generator, it outputs 1.17 V under 4 Suns irradiation, enough to drive a small fan via photo‐thermo‐electric conversion ...
Ning‐Ning Zhang +7 more
wiley +1 more source
Electrostatic adhesion mitigates aerodynamic losses from gap formations in feathered wings. [PDF]
Commun EngHaughn KPT +3 more
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Aerodynamic Effects of a Blended Multi-Winglet on an Airliner in Subsonic and Transonic Regimes. [PDF]
Biomimetics (Basel)Kobayashi E +3 more
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Numerical simulation of the transition flight aerodynamics of cross-shaped quad-tiltrotor UAV. [PDF]
Sci RepDu S, Zha Y.
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MHD Maxwell dusty fluid in thermally stratified radiative flow with temperature-dependent thermal conductivity and Cattaneo-Christov model. [PDF]
HeliyonRaghu A, Gajjela N, Garvandha M.
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Research on a Multi-Dimensional Information Fusion Mechanical Wear Fault-Diagnosis Algorithm Based on Data Regeneration. [PDF]
Sensors (Basel)Zhou Q +7 more
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Effect of Slip Flow on Aerodynamics
, 2019 This paper presents the effect different of slip boundary conditions on aerodynamics. The effect of continuum breakdown on aerodynamics of lift wing was shown. Present results keep an agreement with the results in reference about flow around the cylinder.
Fei Huang +3 more
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Effect of rear-fuselage design on the aerodynamics of a helicopter at side-slip angle
Aerospace Science and Technology, 2019 Abstract The aerodynamic design of a helicopter fuselage encounters many complexities that arise from the large variation in side-slip angle during different flight maneuvers and gusty conditions. A wind tunnel investigation was performed on a scaled-down helicopter model at Reynolds number of Re w = 9.6 × 10 5 to analyze its ...
Drew Gingras +3 more
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Unsteady Aerodynamics Simulation of A Road Vehicle Running with Cyclic Yaw and Side-slip Motions
31st AIAA Applied Aerodynamics Conference, 2013 Takuji Nakashima +3 more
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