Change search
ReferencesLink to record
Permanent link

Direct link
Flow Processes in Rocket Engine Nozzles with Focus on Flow Separation and Side-Loads
KTH, Superseded Departments, Mechanics.
2002 (English)Licentiate thesis, comprehensive summary (Other scientific)
Place, publisher, year, edition, pages
Stockholm: Mekanik , 2002. , 122 p.
Trita-MEK, ISSN 0348-467X ; 2002:09
Keyword [en]
turbulent, boundary layer, shock wave, interaction, intermittent, overexpanded, rocket nozzle, flow separation, side-load, models, criteria, prediction, review
URN: urn:nbn:se:kth:diva-1452ISBN: OAI: diva2:7328
NR 20140805Available from: 2002-06-25 Created: 2002-06-25Bibliographically approved

Open Access in DiVA

fulltext(9327 kB)10043 downloads
File information
File name FULLTEXT01.pdfFile size 9327 kBChecksum SHA-1
Type fulltextMimetype application/pdf

By organisation

Search outside of DiVA

GoogleGoogle Scholar
Total: 10043 downloads
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

Total: 914 hits
ReferencesLink to record
Permanent link

Direct link