Turbulent boundary-layer growth far downstream in a slowly expanding hypersonic nozzle /
| dc.contributor.author | Chang, Lu-chung, | en_US |
| dc.date.accessioned | 2013-08-16T12:24:36Z | |
| dc.date.available | 2013-08-16T12:24:36Z | |
| dc.date.issued | 1971 | en_US |
| dc.identifier.uri | https://hdl.handle.net/11244/3038 | |
| dc.format.extent | x, 85 leaves : | en_US |
| dc.publisher | The University of Oklahoma. | en_US |
| dc.subject | Aerodynamics, Hypersonic. | en_US |
| dc.subject | Supersonic nozzles. | en_US |
| dc.subject | Engineering, Aerospace. | en_US |
| dc.title | Turbulent boundary-layer growth far downstream in a slowly expanding hypersonic nozzle / | en_US |
| dc.type | Thesis | en_US |
| dc.thesis.degree | D.Engr. | en_US |
| dc.note | Source: Dissertation Abstracts International, Volume: 32-12, Section: B, page: 6986. | en_US |
| ou.identifier | (UMI)AAI7127602 | en_US |
| ou.group | Other |
Files in this item
This item appears in the following Collection(s)
-
OU - Dissertations [9418]