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

Transpiration Cooling Models applied to Rocket Combustion Chambers

Selzer, Markus and Schweikert, Sven and von Wolfersdorf, Jens and Hald, Hermann (2012) Transpiration Cooling Models applied to Rocket Combustion Chambers. Project Report.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/79732/
Document Type:Monograph (Project Report)
Title:Transpiration Cooling Models applied to Rocket Combustion Chambers
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Selzer, MarkusDLR BKUNSPECIFIED
Schweikert, SvenITLRUNSPECIFIED
von Wolfersdorf, JensITLRUNSPECIFIED
Hald, HermannDLR BKUNSPECIFIED
Date:November 2012
Journal or Publication Title:Transregio 40 Annal Report
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:transpiration cooling, rocket combustion chamber
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:other
DLR - Research area:Raumfahrt
DLR - Program:R - no assignment
DLR - Research theme (Project):R - no assignment
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Space Structural Components
Deposited By: Selzer, Markus
Deposited On:18 Dec 2012 08:23
Last Modified:18 Dec 2012 08:23

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.