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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 on Numerical Fluid Mechanics and Multidisciplinary Design Notes, Vol. 96. Springer Verlag Berlin, Heidelberg, New York. pp. 317-323. ISBN 978-3-540-74458-0.
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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.
| Document Type: | Contribution to a Collection | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Title: | Experimental Investigation and Numerical Simulation on a Missile Radome at Mach 6 | ||||||||||||
| Authors: |
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| Date: | 2008 | ||||||||||||
| Journal or Publication Title: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design | ||||||||||||
| Refereed publication: | Yes | ||||||||||||
| In ISI Web of Science: | No | ||||||||||||
| Volume: | Vol. 96 | ||||||||||||
| Page Range: | pp. 317-323 | ||||||||||||
| Editors: |
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| Publisher: | Springer Verlag Berlin, Heidelberg, New York | ||||||||||||
| Series Name: | Notes | ||||||||||||
| 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: | L AR - Aircraft Research | ||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||
| DLR - Research theme (Project): | L - Military Technologies | ||||||||||||
| Location: | Göttingen | ||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Spacecraft | ||||||||||||
| Deposited By: | Dagmar Brennecke-Hosseinzadeh | ||||||||||||
| Deposited On: | 15 Jan 2009 | ||||||||||||
| Last Modified: | 27 Apr 2009 13:12 |
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