Numerical Investigation of Boundary Layer Instability and Transition Induced by Rotating Wall-normal Cylindrical Roughness Elements
Title | Numerical Investigation of Boundary Layer Instability and Transition Induced by Rotating Wall-normal Cylindrical Roughness Elements PDF eBook |
Author | Yongxiang Wu |
Publisher | |
Pages | 0 |
Release | 2022 |
Genre | |
ISBN | 9783843952101 |
New Results in Numerical and Experimental Fluid Mechanics XIV
Title | New Results in Numerical and Experimental Fluid Mechanics XIV PDF eBook |
Author | Andreas Dillmann |
Publisher | Springer Nature |
Pages | 700 |
Release | 2023-10-24 |
Genre | Technology & Engineering |
ISBN | 3031404823 |
This book offers timely insights into research on numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications. It reports on findings by members of the Deutsche Strömungsmechanische Arbeitsgemeinschaft, STAB (German Aerodynamics/Fluid Mechanics Association) and the Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal Oberth e.V., DGLR (German Society for Aeronautics and Astronautics) and covers both nationally and EC-funded projects. Continuing on the tradition of the previous volumes, the book highlights innovative solutions, promoting translation from fundamental research to industrial applications. It addresses academics and professionals in the field of aeronautics, astronautics, ground transportation, and energy alike.
New Results in Numerical and Experimental Fluid Mechanics XII
Title | New Results in Numerical and Experimental Fluid Mechanics XII PDF eBook |
Author | Andreas Dillmann |
Publisher | Springer Nature |
Pages | 867 |
Release | 2019-09-26 |
Genre | Technology & Engineering |
ISBN | 3030252531 |
This book gathers contributions to the 21st biannual symposium of the German Aerospace Aerodynamics Association (STAB) and the German Society for Aeronautics and Astronautics (DGLR). The individual chapters reflect ongoing research conducted by the STAB members in the field of numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications, and cover both nationally and EC-funded projects. Special emphasis is given to collaborative research projects conducted by German scientists and engineers from universities, research-establishments and industries. By addressing a number of cutting-edge applications, together with the relevant physical and mathematics fundamentals, the book provides readers with a comprehensive overview of the current research work in the field. The book’s primary emphasis is on aerodynamic research in aeronautics and astronautics, and in ground transportation and energy as well.
Scientific and Technical Aerospace Reports
Title | Scientific and Technical Aerospace Reports PDF eBook |
Author | |
Publisher | |
Pages | 836 |
Release | 1994 |
Genre | Aeronautics |
ISBN |
Applied Mechanics Reviews
Title | Applied Mechanics Reviews PDF eBook |
Author | |
Publisher | |
Pages | 1096 |
Release | 1961 |
Genre | Mechanics, Applied |
ISBN |
Numerical Study of Boundary Layer Instability of Flow Over Axisymmetric Cylinder
Title | Numerical Study of Boundary Layer Instability of Flow Over Axisymmetric Cylinder PDF eBook |
Author | Kai-Hsiung Kao |
Publisher | |
Pages | 240 |
Release | 1990 |
Genre | Turbulence |
ISBN |
Transition Location Effect on Shock Wave Boundary Layer Interaction
Title | Transition Location Effect on Shock Wave Boundary Layer Interaction PDF eBook |
Author | Piotr Doerffer |
Publisher | Springer Nature |
Pages | 540 |
Release | 2020-07-30 |
Genre | Technology & Engineering |
ISBN | 3030474615 |
This book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction. The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project. The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.