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Experimental Investigation and Numerical Simulation on a Missile Radome at Mach 6

Dankert, Carl and Otto, Hannes (2008) Experimental Investigation and Numerical Simulation on a Missile Radome at Mach 6. In: Notes Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 96. Springer Verlag Berlin, Heidelberg, New York. pp. 317-323. ISBN 978-3-540-74458-0.

Full text not available from this repository.

Abstract

Im HEG Göttingen wurden an einem Flugkörper-Radom Wärmeübergänge und Wanddrücke bei Mach 6 gemessen und mit CFD Rechnungen mit dem TAU-Code verglichen.

Item URL in elib:https://elib.dlr.de/45214/
Document Type:Contribution to a Collection
Title:Experimental Investigation and Numerical Simulation on a Missile Radome at Mach 6
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Dankert, CarlUNSPECIFIEDUNSPECIFIED
Otto, HannesUNSPECIFIEDUNSPECIFIED
Date:2008
Journal or Publication Title:Notes
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 96
Page Range:pp. 317-323
Editors:
EditorsEmail
Tropea, CameronUNSPECIFIED
Jakirlic, SuadUNSPECIFIED
Heinemann, Hans-JoachimUNSPECIFIED
Henke, RolfUNSPECIFIED
Hönlinger, HeinzUNSPECIFIED
Publisher:Springer Verlag Berlin, Heidelberg, New York
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISBN:978-3-540-74458-0
Status:Published
Keywords:Flugkörper, Hyperschall, Wärmeübergang, Radom
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Military Technologies (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Brennecke-Hosseinzadeh, Dagmar
Deposited On:15 Jan 2009
Last Modified:22 Jan 2018 16:50

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