Adelaide Research & Scholarship
Please use this identifier to cite or link to this item:
http://hdl.handle.net/2440/43531| Citations | ||
| Scopus | Web of Science® | Altmetric |
|---|---|---|
|
?
|
?
|
|
| Type: | Journal article |
| Title: | Steady-state high pressure LOx/H2 rocket engine combustion |
| Author: | Smith, Joshua John Schneider, Gerald Manfred Suslov, D. Oschwald, M. Haidn, O. |
| Citation: | Aerospace Science and Technology, 2007; 11 (1):39-47 |
| Part of: | Propellant combustion phenomena / Luigi T. DeLuca, Paul Kuentzmann and Alexander S. Rudakov (eds.) |
| Publisher: | Editions Scientifiques Medicales Elsevier |
| Issue Date: | 2007 |
| ISSN: | 1270-9638 |
| School/Discipline: | School of Mechanical Engineering |
| Statement of Responsibility: | Joshua J. Smith, Gerald Schneider, Dmitry Suslov, Michael Oschwald and Oskar Haidn |
| Description: | Copyright © 2006 Elsevier Masson SAS All rights reserved. |
| RMID: | 0020070439 |
| DOI: | 10.1016/j.ast.2006.08.007 |
| Description (link): | http://www.elsevier.com/wps/find/journaldescription.cws_home/600735/description#description |
| Appears in Collections: | Mechanical Engineering publications |
Files in This Item:
There are no files associated with this item.
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.
