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Towards effective flow control and mitigation of shock effects in aeronautical applications

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Towards effective flow control and mitigation of shock effects in aeronautical applications/ edited by Pawel Flaszynski, Holger Babinsky, Piotr Doerffer.
其他作者:	Doerffer, Piotr.
出版者:	Cham :Springer Nature Switzerland : : 2025.,
面頁冊數:	x, 380 p. :ill. (some col.), digital ; : 24 cm.;
Contained By:	Springer Nature eBook
標題:	Computational Physics and Simulations. -
電子資源:	https://doi.org/10.1007/978-3-031-86605-0
ISBN:	9783031866050

Towards effective flow control and mitigation of shock effects in aeronautical applications
Towards effective flow control and mitigation of shock effects in aeronautical applications[electronic resource] /edited by Pawel Flaszynski, Holger Babinsky, Piotr Doerffer. - Cham :Springer Nature Switzerland :2025. - x, 380 p. :ill. (some col.), digital ;24 cm. - Notes on numerical fluid mechanics and multidisciplinary design,v. 2011860-0824 ;. - Notes on numerical fluid mechanics and multidisciplinary design ;v. 104 .

Part1.Introduction -- Part2.Numerical and experimental methods development -- 1."From high-fidelity high-order to reduced-order modeling for unsteady shock wave/boundary layer interactions " -- 2.Numerical tools for high-fidelity simulation of sblis -- 3."Development of a PVDF Piezo-Film Sensor for Unsteady Wall-Pressure Measurements in sblis" -- Part3.Transitional/turbulent SBLI and flow control -- 4.Non-linearities in the low-frequency dynamics of transitional SBLI -- 5.The length and time scales of transitional sblis -- 6."Parameter Influence on Porous Bleed Performance for Shock-Wave/Boundary-Layer Interaction Control" -- 7.Unsteady three-dimensional oblique shock wave boundary-layer interactions -- 8.Oblique-shock wave boundary layer interactions control: shock control bumps -- Part4.Airfoil/wing configuration -- 9.Numerical Study of Unsteady Shock/Boundary Layer Interaction -- 10.Numerical study and physical analysis of the transonic interaction and its modification through morphing around supercritical wings at high Reynolds number -- Part5.Transonic compressor -- 11.Numerical investigations of transitional SBLI on a highly loaded-transonic compressor -- 12.Reynolds number effects on shock wave boundary layer interaction in highly loaded compressor stator -- 13."Experimental and Numerical Investigations of SBLI and Flow Control on a Transonic Compressor Cascade " -- 14.Surface roughness effect on SBLI on compressor rotor profile -- 15."Shock Oscillation Mechanisms of Highly Separated Transitional Shock-Wave/Boundary-Layer Interactions".

Open access.

This open-access book reports on both experimental and numerical findings from the H2020-funded project TEAMAero (Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications). It covers novel contributions on improving the fundamental understanding of the physics of shock wave boundary layer interaction, developments in ﬂow control for mitigation of shock effects, and advanced numerical methods for predicting those effects. All in all, this book offers a timely snapshot of research and developments in numerical methods for flow analysis and control, with a special emphasis on high-speed flows. It offers extensive information to both researchers and professionals.

ISBN: 9783031866050

Standard No.: 10.1007/978-3-031-86605-0doiSubjects--Topical Terms:

1366360
Computational Physics and Simulations.

LC Class. No.: TL570

Dewey Class. No.: 629.1323

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506 $a Open access.
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