Drag reduction by a multi-point optimised hybrid flow control method for two supercritical airfoils-Reference-Cited by-同舟云学术

Drag reduction by a multi-point optimised hybrid flow control method for two supercritical airfoils

Published:2016-09-02 Issue:5 Volume:25 Page:359-387
ISSN:1779-7179
Container-title:European Journal of Computational Mechanics
language:en
Short-container-title:European Journal of Computational Mechanics

Author:

Nejati A.¹,Mazaheri K.¹

Affiliation:

1. Center of Excellence in Aerospace Systems, Sharif University of Technology, Tehran, Iran

Publisher

River Publishers

Subject

Mechanical Engineering,Mechanics of Materials,Modeling and Simulation

Link

https://www.tandfonline.com/doi/pdf/10.1080/17797179.2016.1240535

Reference20 articles.

1. Balleur, J. C., Girodroux-Lavigne, P. & Gassot, H. (1999). Prediction of transonic airfoil/wing flow with control using time-accurate viscous-inviscid interaction approach (Results of Project EUROSHOCK II Supported by the European Union 1996–1999, 3rd Annual Report). Berlin: Springer. doi: 10.1007/978-3-540-45856-2_9

2. Birkemeyer, J. (1999). Drag minimization on a transonic wing by ventilation and adaptive contour bump (DLR Research Report 1999–28). Ph.D. Thesis University Hannover, Hannover.

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