Turbulent boundary-layer growth far downstream in a slowly expanding hypersonic nozzle /

dc.contributor.authorChang, Lu-chung,en_US
dc.date.accessioned2013-08-16T12:24:36Z
dc.date.available2013-08-16T12:24:36Z
dc.date.issued1971en_US
dc.format.extentx, 85 leaves :en_US
dc.identifier.urihttp://hdl.handle.net/11244/3038
dc.noteSource: Dissertation Abstracts International, Volume: 32-12, Section: B, page: 6986.en_US
dc.publisherThe University of Oklahoma.en_US
dc.subjectAerodynamics, Hypersonic.en_US
dc.subjectSupersonic nozzles.en_US
dc.subjectEngineering, Aerospace.en_US
dc.thesis.degreeD.Engr.en_US
dc.titleTurbulent boundary-layer growth far downstream in a slowly expanding hypersonic nozzle /en_US
dc.typeThesisen_US
ou.groupOther
ou.identifier(UMI)AAI7127602en_US

Files

Original bundle
Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
7127602.PDF
Size:
1.45 MB
Format:
Adobe Portable Document Format