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Comparison of High Pressure h2/O2 Rocket Model-Engine 2D-Reference-Simulation Results
Schley, C.-A. and Golovitchev, V. and Hagemann, G. (1995) Comparison of High Pressure h2/O2 Rocket Model-Engine 2D-Reference-Simulation Results. In: AIAA. 31st AIAA Joint Propulsion Conference and Exhibit July 10-12, 1995 / San Diego, CA.
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| Document Type: | Conference or Workshop Item (Paper) | ||||||||
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| Additional Information: | institution=AIAA, LIDO-Berichtsjahr=1995, pages=11, | ||||||||
| Title: | Comparison of High Pressure h2/O2 Rocket Model-Engine 2D-Reference-Simulation Results | ||||||||
| Authors: |
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| Date: | 1995 | ||||||||
| Journal or Publication Title: | AIAA | ||||||||
| Series Name: | AIAA-95-2429 | ||||||||
| Status: | Published | ||||||||
| Keywords: | Rocket Combustion Chamber, Numerical Simulation, 2D Geometry, Coaxial Injection, Physical Sub Models | ||||||||
| Event Title: | 31st AIAA Joint Propulsion Conference and Exhibit July 10-12, 1995 / San Diego, CA | ||||||||
| HGF - Research field: | UNSPECIFIED | ||||||||
| HGF - Program: | Space | ||||||||
| HGF - Program Themes: | W RP - Raumtransport | ||||||||
| DLR - Research area: | UNSPECIFIED | ||||||||
| DLR - Program: | W RP - Raumtransport | ||||||||
| DLR - Research theme (Project): | E -- no assignement | ||||||||
| Location: | Lampoldshausen | ||||||||
| Institutes and Institutions: | Institute of Space Propulsion | ||||||||
| Deposited By: | elib DLR-Beauftragter | ||||||||
| Deposited On: | 02 Apr 2006 | ||||||||
| Last Modified: | 27 Apr 2009 05:37 |
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