Results 1 to 10 of about 90,147 (210)

Nonlinear Modeling the Quadcopter Considering the Aerodynamic Interaction [PDF]

open access: yesIEEE Access, 2021
This paper presents a nonlinear model of the quadcopter to simulate the actual motion. An aerodynamic model of the rotor is obtained through wind-tunnel tests, which consider the variations in the rotor’s angular velocity, incoming flow speed, and
Jianchuan Ye   +4 more
doaj   +2 more sources

Computational Study of Propeller–Wing Aerodynamic Interaction [PDF]

open access: yesAerospace, 2018
Kestrel simulation tools are used to investigate the mutual interference between the propeller and wing of C130J aircraft. Only the wing, nacelles, and propeller geometries are considered.
Pooneh Aref   +4 more
doaj   +2 more sources

The Aerodynamic Interaction Effects between the Rotor and Fuselage on the Drag Performance of a Civil Helicopter in Forward Flight

open access: yesApplied Sciences, 2023
The aerodynamic interaction between the rotor and fuselage is an important consideration in relation to the drag performance prediction of helicopters. In this paper, based on dynamic patched-grid technology coupled with a three-dimensional N–S equation ...
Wenbo Shi, Heng Zhang, Yuanxiang Li
doaj   +3 more sources

PROBLEMOFAERODYNAMIC INTERACTION OF TRAFFIC STREAMS [PDF]

open access: yesTransport Problems, 2020
Thisstudy presents amodel of continuous oncoming traffic flows of vehiclesalong highways. The flow of atmospheric air and impurityparticlesis modeled numerically based onunsteadyReynolds-Averaged Navier–Stokesequations using the MTFS ...
Valerii SOLODOV
doaj   +1 more source

Effect of Ducted Multi-Propeller Configuration on Aerodynamic Performance in Quadrotor Drone

open access: yesDrones, 2021
Motivated by a bioinspired optimal aerodynamic design of a multi-propeller configuration, here we propose a ducted multi-propeller design to explore the improvement of lift force production and FM efficiency in quadrotor drones through optimizing the ...
Yi Li, Koichi Yonezawa, Hao Liu
doaj   +1 more source

Study on the Aerothermoelastic Characteristics of a Body Flap Considering the Nozzle–Jet Interference

open access: yesAerospace, 2023
A body flap/RCS-integrated configuration is often used to achieve pitch trimming and controlled flight in near space for hypersonic vehicles. Under the high temperature and pressure load induced by the expansion wave at the nozzle exit, the body flap is ...
Ruhao Hua, Qi Chen, Zhao Wan, Hao Chen
doaj   +1 more source

Multiple-Fidelity Modeling of Interactional Aerodynamics [PDF]

open access: yesJournal of Aircraft, 2017
The interaction of trailing vortices with lifting surfaces is investigated using two levels of modeling fidelity. An overset mesh-based Reynolds-averaged Navier–Stokes solver is considered as the high-fidelity computational model. A lower-fidelity model is developed by combining a vortex panel method with a propeller aerodynamic model and slipstream ...
Asitav Mishra   +2 more
openaire   +1 more source

Influence of Aerodynamic Interaction on Performance of Contrarotating Propeller/Wing System

open access: yesAerospace, 2022
This paper gives a quantitative account of the influence of slipstream on the aerodynamic performance of a contrarotating propeller (CRP)/wing system, and compares it with the CRP and clean wing. To accurately evaluate the complex aerodynamic interaction,
Zhitao Zhang   +3 more
doaj   +1 more source

Analysis on the Propeller Slipstream Interference with Autorotating Rotor Aerodynamic Characteristics

open access: yesHangkong gongcheng jinzhan, 2020
The propeller slipstream passed through the rotor plane when the autogyro is flying forward, will produce the unsteady aerodynamic interference on the autorotating rotor.
WU Weiwei, MA Cunwang, SUN Kaijun
doaj   +1 more source

Unsteady loads for coaxial rotors in forward flight computed using a vortex particle method [PDF]

open access: yes, 2018
Recent advances in coaxial rotor design have shown benefits of this configuration. Nevertheless, issues related to rotor-head drag, aerodynamic performance, wake interference, and vibration should also be considered.
Barakos, George   +2 more
core   +1 more source

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