2011
DOI: 10.1007/s11433-011-4284-2
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Wing tip vortex structure behind an airfoil with flaps at the tip

Abstract: In this work, the wing tip vortex structure behind a NACA 0015 airfoil with and without small flaps was studied using a Partical Image Velocimetry (PIV) system. The experiment was carried out in a low speed wind tunnel with a test section of 0.5 m × 0.5 m. The Reynolds number (Re), defined by the chord length of the wing (C), was 8.1×10 4 . The angle of attack was fixed at 10°. The PIV measurements were made from 0 to 2C, measured from the trailing edge of the model. The dihedral angle of three flaps was 15°,… Show more

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Cited by 7 publications
(1 citation statement)
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“…The related work is made for the control of large angle maneuvers for the flexible solar sail [31] and optimal four-impulse rendezvous between coplanar elliptical orbits [32]. The wing tip vortex structure behind an airfoil with flaps at the tip of the aircraft has been studied by simulation and experimental work [33]. For the discovering plan on the Moon and to the remote planets, some numerical and theoretical progress has been made related to the design and optimization of a trajectory for Moon departure Near Earth Asteroid exploration [34], and fuel optimal low thrust rendezvous with outer planets via gravity assist [35].…”
Section: The Theory and Simulation Work On Aerospace Engineering At Hmentioning
confidence: 99%
“…The related work is made for the control of large angle maneuvers for the flexible solar sail [31] and optimal four-impulse rendezvous between coplanar elliptical orbits [32]. The wing tip vortex structure behind an airfoil with flaps at the tip of the aircraft has been studied by simulation and experimental work [33]. For the discovering plan on the Moon and to the remote planets, some numerical and theoretical progress has been made related to the design and optimization of a trajectory for Moon departure Near Earth Asteroid exploration [34], and fuel optimal low thrust rendezvous with outer planets via gravity assist [35].…”
Section: The Theory and Simulation Work On Aerospace Engineering At Hmentioning
confidence: 99%