|
Showing 1 - 3 of
3 matches in All Departments
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.
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.
|
|