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Investigation of Hypersonic Boundary-Layer Transition Using High-Speed Visualization Techniquesment

Laurence, Stuart and Wagner, Alexander and Hannemann, Klaus (2015) Investigation of Hypersonic Boundary-Layer Transition Using High-Speed Visualization Techniquesment. Springer International Publishing. ISBN 978-3-319-16834-0.

Full text not available from this repository.

Official URL: http://www.springer.com/us/book/9783319168340

Abstract

Transition from laminar to turbulent flow in hypersonic boundary layers leads to highly elevated levels of surface heat transfer and frictional drag.

Item URL in elib:https://elib.dlr.de/100669/
Document Type:Proceedings
Additional Information:Book Part: Part VII, Online ISBN: 978-3-319-16835-7
Title:Investigation of Hypersonic Boundary-Layer Transition Using High-Speed Visualization Techniquesment
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Laurence, Stuartstuart.laurence (at) umd.eduUNSPECIFIED
Wagner, Alexanderalexander.wagner (at) dlr.deUNSPECIFIED
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Date:2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:1
DOI :10.1007/978-3-319-16835-7_107
Page Range:pp. 671-676
Editors:
EditorsEmail
Bonazza, RiccardoDepartment of Engineering Physics, University of Wisconsin
Ranjan, DeveshDepartment of Mechanical Engineering, Georgia Institute of Technology
Publisher:Springer International Publishing
ISBN:978-3-319-16834-0
Status:Published
Keywords:High Enthalpy Shock Tunnel (HEG), boundary-layer, transition
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Anlagen u. Messtechnik
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Micknaus, Ilka
Deposited On:16 Dec 2015 09:00
Last Modified:10 May 2016 23:37

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