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Beschreibung

Hypersonic turbulent boundary layers are a fundamental phenomenon in high-speed flight. The interaction of shock waves with hypersonic turbulent boundary layers has a critical impact on vehicle aerothermodynamic loading including surface heat transfer, pressure and skin friction. This book provides a comprehensive exposition of hypersonic turbulent boundary layers, including the fundamental mathematical theory, structure of equilibrium boundary layers, and extensive surveys of Direct Numerical Simulation (DNS), Large Eddy Simulation (LES) and experiments. It also provides a roadmap for both future experiments and DNS and LES simulations. Descriptions of hypersonic ground test facilities is included as an appendix. As a research and reference text, this book would appeal to graduate students and researchers in hypersonics and could be the basis for professional training courses.

Key Features

  • Provides a summary of the state-of-the-art of experimental knowledge of hypersonic turbulent boundary layers
  • Summarises the state-of-the-art of Direct Numerical and Large Eddy Simulation of hypersonic turbulent boundary layers
  • Provides a roadmap for future experimental and DNS and LES research in hypersonic turbulent boundary layers
  • Includes a brief summary of experimental hypersonic test facilities
  • Written by experts in the field

Hypersonic turbulent boundary layers are a fundamental phenomenon in high-speed flight. The interaction of shock waves with hypersonic turbulent boundary layers has a critical impact on vehicle aerothermodynamic loading including surface heat transfer, pressure and skin friction. This book provides a comprehensive exposition of hypersonic turbulent boundary layers, including the fundamental mathematical theory, structure of equilibrium boundary layers, and extensive surveys of Direct Numerical Simulation (DNS), Large Eddy Simulation (LES) and experiments. It also provides a roadmap for both future experiments and DNS and LES simulations. Descriptions of hypersonic ground test facilities is included as an appendix. As a research and reference text, this book would appeal to graduate students and researchers in hypersonics and could be the basis for professional training courses.

Key Features

  • Provides a summary of the state-of-the-art of experimental knowledge of hypersonic turbulent boundary layers
  • Summarises the state-of-the-art of Direct Numerical and Large Eddy Simulation of hypersonic turbulent boundary layers
  • Provides a roadmap for future experimental and DNS and LES research in hypersonic turbulent boundary layers
  • Includes a brief summary of experimental hypersonic test facilities
  • Written by experts in the field
Details
Erscheinungsjahr: 2023
Fachbereich: Mechanik & Akustik
Genre: Importe, Physik
Rubrik: Naturwissenschaften & Technik
Medium: Buch
Reihe: IOP ebooks
Inhalt: Gebunden
ISBN-13: 9780750350006
ISBN-10: 0750350008
Sprache: Englisch
Einband: Gebunden
Autor: Knight, Doyle
Kianvashrad, Nadia
Hersteller: Institute of Physics Publishing
IOP ebooks
Verantwortliche Person für die EU: Libri GmbH, Europaallee 1, D-36244 Bad Hersfeld, gpsr@libri.de
Maße: 261 x 182 x 39 mm
Von/Mit: Doyle Knight (u. a.)
Erscheinungsdatum: 29.06.2023
Gewicht: 1,364 kg
Artikel-ID: 123502930