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Simulation of Missiles with Grid Fins using Unstructured Navier-Stokes Solver coupled to a Semi-Empirical Actuator Disc

Reynier, Ph. and Schülein, E. and Longo, J.M. (2003) Simulation of Missiles with Grid Fins using Unstructured Navier-Stokes Solver coupled to a Semi-Empirical Actuator Disc. International Symposium “Integrating CFD and Experiments”, 8-9 September 2003, Glasgow, UK,.

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Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2003,
Title:Simulation of Missiles with Grid Fins using Unstructured Navier-Stokes Solver coupled to a Semi-Empirical Actuator Disc
Authors:
AuthorsInstitution or Email of Authors
Reynier, Ph.UNSPECIFIED
Schülein, E.UNSPECIFIED
Longo, J.M.UNSPECIFIED
Date:2003
Volume:Proceedings of the International Symposium "Integrating CFD and Experiments", Glaskow, UK, 2003
Status:Published
Keywords:Grid-fins, missile, force, software tool, TAU-Code
Event Title:International Symposium “Integrating CFD and Experiments”, 8-9 September 2003, Glasgow, UK,
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: elib DLR-Beauftragter
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:16

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