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Determination of Velocity Fields in a LOX/GH2-Rocket Model Combustor by Using the Droplet Tracking Velocimetry.

Barsacq, M. (1997) Determination of Velocity Fields in a LOX/GH2-Rocket Model Combustor by Using the Droplet Tracking Velocimetry. DLR-Interner Bericht. 645-97/14, 34 S.

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Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1997,
Title:Determination of Velocity Fields in a LOX/GH2-Rocket Model Combustor by Using the Droplet Tracking Velocimetry.
Authors:
AuthorsInstitution or Email of Authors
Barsacq, M.UNSPECIFIED
Date:1997
Number of Pages:34
Status:Published
Keywords:Turbulent reactive flows; 2-phase flows with combustion
HGF - Research field:UNSPECIFIED
HGF - Program:Space (old)
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 05:42

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