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您的检索式：作者名="G.Eitelberg"
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| 1 | Design and numerical investigation of swirl recovery vanes for the Fokker 29 propeller显示文摘Swirl recovery vanes(SRVs) are a set of stationary vanes located downstream from a propeller, which may recover some of the residual swirl from the propeller, hoping for an improvement in both thrust and efficiency. The SRV concept design for a scaled version representing the Fokker 29 propeller is performed in this paper, which may give rise to a promotion in propulsive performance of this traditional propeller. Firstly the numerical strategy is validated from two aspects of global quantities and the local flow field of the propeller compared with experimental data, and then the exit flow together with the development of propeller wake is analyzed in detail.Three kinds of SRV are designed with multiple circular airfoils. The numerical results show that the swirl behind the propeller is recovered significantly with Model V3, which is characterized by the highest solidity along spanwise, for various working conditions, and the combination of rotor and vane produced 5.76% extra thrust at the design point. However, a lower efficiency is observed asking for a better vane design and the choice of a working point. The vane position is studied which shows that there is an optimum range for higher thrust and efficiency. | Wang Yangang Li Qingxi G.Eitelberg L.L.M.Veldhuis M.Kotsonis | 2014 | Chinese Journal of Aeronautics2014，27，5： | 2 |
| 2 | An investigation of tip vortices unsteady interaction for Fokker 29 propeller with swirl recovery vane显示文摘A numerical study was performed to explore the unsteady interaction between the upstream propeller and the downstream swirl recovery vane(SRV) by transient simulations. Much larger fluctuations of thrust coefficient were observed on the vane, which indicates that the variations of the total efficiency depend mainly on the working performance of the stator. The harmonic loads of the decomposed unsteady blade-surface pressures show that the stator experiences about ten times higher of unsteadiness compared with the rotor. Notable changes appear at the vane leading edge due to the potential disturbance as well as the sweeping effects from the wake of the upstream propeller, whereas more significant unsteadiness occurs at the stator tip region as a result of the interaction between the rotor/stator tip vortices. The visualization of vortex structures addresses that the rotor tip vortex has a dominant effect on the stator tip vortex since the latter one starts right at the impingement location on the vane top in this configuration. Furthermore,a longer and a shorter SRV were investigated based on the original case to explore different interaction patterns for the rotor/stator tip vortices. Weaker effects have been observed as expected. | Li Qingxi Wang Yangang G.Eitelberg | 2016 | Chinese Journal of Aeronautics2016，29，1： | 1 |
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