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Pawel Flaszynski | Akateeminen Kirjakauppa

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Transition Location Effect on Shock Wave Boundary Layer Interaction - Experimental and Numerical Findings from the TFAST Project
Piotr Doerffer; Pawel Flaszynski; Jean-Paul Dussauge; Holger Babinsky; Patrick Grothe; Anna Petersen; Flavien Billard
Springer Nature Switzerland AG (2020)
Kovakantinen kirja
129,90
Tuotetta lisätty
ostoskoriin kpl
Siirry koriin
Transition Location Effect on Shock Wave Boundary Layer Interaction - Experimental and Numerical Findings from the TFAST Project
Piotr Doerffer; Pawel Flaszynski; Jean-Paul Dussauge; Holger Babinsky; Patrick Grothe; Anna Petersen; Flavien Billard
Springer Nature Switzerland AG (2021)
Pehmeäkantinen kirja
129,90
Tuotetta lisätty
ostoskoriin kpl
Siirry koriin
Smart Morphing and Sensing for Aeronautical Configurations : Prototypes, Experimental and Numerical Findings from the H2020 N° 7
Marianna Braza (ed.); Jean-François Rouchon (ed.); George Tzabiras (ed.); Franco Auteri (ed.); Pawel Flaszynski (ed.)
Springer (2023)
Kovakantinen kirja
147,10
Tuotetta lisätty
ostoskoriin kpl
Siirry koriin
Smart Morphing and Sensing for Aeronautical Configurations : Prototypes, Experimental and Numerical Findings from the H2020 N° 7
Marianna Braza (ed.); Jean-François Rouchon (ed.); George Tzabiras (ed.); Franco Auteri (ed.); Pawel Flaszynski (ed.)
Springer (2024)
Pehmeäkantinen kirja
147,10
Tuotetta lisätty
ostoskoriin kpl
Siirry koriin
Transition Location Effect on Shock Wave Boundary Layer Interaction - Experimental and Numerical Findings from the TFAST Project
129,90 €
Springer Nature Switzerland AG
Sivumäärä: 540 sivua
Asu: Kovakantinen kirja
Painos: 1st ed. 2021
Julkaisuvuosi: 2020, 31.07.2020 (lisätietoa)
Kieli: Englanti
Tuotesarja: Notes on Numerical Fluid Mechanics and Multidisciplinary Design 144
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.

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Tilaustuote | Arvioimme, että tuote lähetetään meiltä noin 4-5 viikossa | Tilaa jouluksi viimeistään 27.11.2024
Myymäläsaatavuus
Helsinki
Tapiola
Turku
Tampere
Transition Location Effect on Shock Wave Boundary Layer Interaction - Experimental and Numerical Findings from the TFAST Projectzoom
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ISBN:
9783030474607
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