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Advances in Effective Flow Separation Control for Aircraft Drag Reduction [electronic resource] : Modeling, Simulations and Experimentations / edited by Ning Qin, Jacques Periaux, Gabriel Bugeda.

Contributor(s): Qin, Ning [editor.] | Periaux, Jacques [editor.] | Bugeda, Gabriel [editor.] | SpringerLink (Online service).
Material type: materialTypeLabelBookSeries: Computational Methods in Applied Sciences: 52Publisher: Cham : Springer International Publishing : Imprint: Springer, 2020Edition: 1st ed. 2020.Description: X, 341 p. 285 illus., 218 illus. in color. online resource.Content type: text Media type: computer Carrier type: online resourceISBN: 9783030296889.Subject(s): Aerospace engineering | Astronautics | Fluid mechanics | Mathematical physics | Mathematical optimization | Aerospace Technology and Astronautics | Engineering Fluid Dynamics | Theoretical, Mathematical and Computational Physics | OptimizationAdditional physical formats: Printed edition:: No title; Printed edition:: No title; Printed edition:: No titleDDC classification: 629.1 Online resources: Click here to access online In: Springer Nature eBookSummary: This book presents the results of a European-Chinese collaborative research project, Manipulation of Reynolds Stress for Separation Control and Drag Reduction (MARS), including an analysis and discussion of the effects of a number of active flow control devices on the discrete dynamic components of the turbulent shear layers and Reynolds stress. From an application point of view, it provides a positive and necessary step to control individual structures that are larger in scale and lower in frequency compared to the richness of the temporal and spatial scales in turbulent separated flows.
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This book presents the results of a European-Chinese collaborative research project, Manipulation of Reynolds Stress for Separation Control and Drag Reduction (MARS), including an analysis and discussion of the effects of a number of active flow control devices on the discrete dynamic components of the turbulent shear layers and Reynolds stress. From an application point of view, it provides a positive and necessary step to control individual structures that are larger in scale and lower in frequency compared to the richness of the temporal and spatial scales in turbulent separated flows.

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