elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

Simultaneous Observation of Liquid Phase Distribution and Flame Front Evolution during the Ignition Transcient of a LOX/GH2-Combustor

Schmidt, V. and McConalogue, B. and Sender, J. and Oschwald, M. (2000) Simultaneous Observation of Liquid Phase Distribution and Flame Front Evolution during the Ignition Transcient of a LOX/GH2-Combustor. In: 9th International Symposium on Flow Visualization, 271-1-271-7. 9th International Symposium on Flow Visualization, Edinburgh, Scotland, August 22-25, 2000.

Full text not available from this repository.

Abstract

Phenomena on millisecond time scale during the transient ignition process in a cryogenic model rocket combustor, like flame propagation, flame/spray interaction, and flame stabilization have not been investigated in detail up to now. Diagnostic techniques developed for characterizing the stationary spray flame are applied to investigate the transient evolution of the LOX-spray and the flame front during the ignition process. Ignition was initiated by focusing a pulsed laser into the combustion chamber. Thus ignition time as well as the position of ignition was well defined. This and the exact control of the delay between ignition and detection time allowed to observe the evolution of the flame front.The distribution of the liquid phase of LOX-droplets have been determined by light-sheet techniques using a double pulsed laser system. Simultaneously the position of the flame front is measured by recordimg the spontaneous emission of the OH-radical. By varying the delay time Pi between ignition and detection in a series of the test runs the transient ignition phenomena have been investigated in the interval from 0 to 5 ms after ignition.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2000, monograph_id=Paper number 271,
Title:Simultaneous Observation of Liquid Phase Distribution and Flame Front Evolution during the Ignition Transcient of a LOX/GH2-Combustor
Authors:
AuthorsInstitution or Email of Authors
Schmidt, V.UNSPECIFIED
McConalogue, B.UNSPECIFIED
Sender, J.UNSPECIFIED
Oschwald, M.UNSPECIFIED
Date:2000
Journal or Publication Title:9th International Symposium on Flow Visualization
Page Range:271-1-271-7
Status:Published
Keywords:cryogenic, rocket engine, laser ignition, spontaneous emission, laser lightsheet
Event Title:9th International Symposium on Flow Visualization, Edinburgh, Scotland, August 22-25, 2000
Organizer:9th International Symposium on Flow Visualization
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
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:16 Sep 2005
Last Modified:06 Jan 2010 13:49

Repository Staff Only: item control page

Browse
Search
Help & Contact
Informationen
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.