Results 21 to 30 of about 3,114 (259)
Contribution to the propeller aerodynamic interference [PDF]
AbstractPropeller wake can significantly change the flowfield at the downstream lifting surfaces and therefore influence its aerodynamic coefficients. The numerical model of the propeller presented here is using discrete vortices to form vortex sheet that is leaving each blade.
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Aerodynamic moment characteristics of tandem-scheme aircraft [PDF]
Aerodynamic interference between forward and back wings of tandem-scheme aircraft significantly affects its pitch and roll moments. The interference increases roll stability in a narrow range of sideslip angles; there is a kink on the dependence of roll ...
Kryvokhatko Illia
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Aerodynamic Interference between Over-Wing-Nacelle and Wing [PDF]
This paper addresses the complex aerodynamic interaction between a rectangular, unswept wing-segment and an over-the-wing mounted ultra-high bypass ratio (UHBR) engine. In the past, various studies have revealed a beneficial interference effect with respect to installation drag due to over-wing-nacelles (OWN).
Lange, Fabian, Kotzem, Michael
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Aerodynamic Optimization of an Over-the-Wing-Nacelle-Mount Configuration
An over-the-wing-nacelle-mount airplane configuration is known to prevent the noise propagation from jet engines toward ground. However, the configuration is assumed to have low aerodynamic efficiency due to the aerodynamic interference effect between a ...
Daisuke Sasaki, Kazuhiro Nakahashi
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Aerodynamic characteristics of vehicles are directly related to their running safety, especially for the high-sided vehicles. In order to study the aerodynamic characteristics under multiple sheltering conditions, a complex large scale (1:20.4) truss ...
Jingyu Zhang +4 more
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Since child aircraft are significantly impacted by the wake interference from the mother aircraft during aerial refueling or the autonomous recovery of unmanned aerial vehicles(UAVs), a rapid prediction model for dual‑aircraft aerodynamic interference is
YUE Hao +4 more
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ADRC Attitude Controller Design for Hypersonic Vehicle based on MIMO-ESO
For the hypersonic vehicle nonlinear attitude mode in reentry process with a strong coupling, aerodynamic parameter perturbations and non-deterministic, combine extended state observer and nonlinear law state error feedback, design the hypersonic vehicle
Wen JianHua, Qin ChangMao, Zhang Xin
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A large-eddy simulation analysis technique is introduced in this paper to determine the interference effect of chamfered square cylinders, which is crucial to predict the impact of wind pressure and load on chamfered high-rise buildings.
Jie Zhang +6 more
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Aerodynamic force measurement algorithm based on U-Net in maglev flight wind tunnel
The aerodynamic force measurement technology during the acceleration phase of the motion model is one of the key technical challenges in the maglev flight wind tunnel. The aerodynamic force measurement balance is subjected to various strong interferences
Guoyao Deng +4 more
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The flight controllability and safety of unmanned compound rotorcraft are closely related to their aerodynamic characteristics. During forward flight, complex aerodynamic interference effects arise among the rotor, propeller, wing, fuselage, and ...
Xinfan Yin +7 more
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