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

Flame Response to Acoustic Excitation in a Rectangular Rocket Combustor with LOx/H2 Propellants

Hardi, Justin (2011) Flame Response to Acoustic Excitation in a Rectangular Rocket Combustor with LOx/H2 Propellants. Institutsseminarreihe, 23. Sep. 2011, Lampoldshausen, Germany. (Unpublished)

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/72877/
Document Type:Conference or Workshop Item (Speech)
Title:Flame Response to Acoustic Excitation in a Rectangular Rocket Combustor with LOx/H2 Propellants
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hardi, JustinJustin.Hardi (at) dlr.dehttps://orcid.org/0000-0003-3258-5261
Date:2011
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:rocket combustion
Event Title:Institutsseminarreihe
Event Location:Lampoldshausen, Germany
Event Type:Other
Event Dates:23. Sep. 2011
Organizer:DLR
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):W - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Technologie
Deposited By: Hanke, Michaela
Deposited On:14 Dec 2011 15:04
Last Modified:01 Dec 2018 19:48

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.