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Navier Stokes Simulation Around a High Velocity Missile with Cross-Flow Jet

Esch, H. and Hitzel, S.M. and Hennig, P. (1998) Navier Stokes Simulation Around a High Velocity Missile with Cross-Flow Jet. In: 82nd Fluid Dynamics Panel Symposium on Missile Aerodynamics, 17.1-17.12. 82nd Fluid Dynamics Panel Symposium on Missile Aerodynamics, Sorrento/Italien, 11.-14. Mai 1998.

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Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Navier Stokes Simulation Around a High Velocity Missile with Cross-Flow Jet
Authors:
AuthorsInstitution or Email of Authors
Esch, H.UNSPECIFIED
Hitzel, S.M.Daimler Benz AG, ATG
Hennig, P.DASA, LFK GmbH
Date:1998
Journal or Publication Title:82nd Fluid Dynamics Panel Symposium on Missile Aerodynamics
Page Range:17.1-17.12
Series Name:RTO-MP-5
Status:Published
Keywords:Navier-Stokes-simulation, cross-flow jet, missile aerodynamics
Event Title:82nd Fluid Dynamics Panel Symposium on Missile Aerodynamics, Sorrento/Italien, 11.-14. Mai 1998
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 20:34

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