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Supersonic asymmetric flutter and divergence of truncated conical shells with ring supported edges
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1971 |
| Description | Supersonic asymmetric flutter and divergence characteristics of truncated conical shells with ring-supported edges under three types of flow-induced instabilities |
| File Size | 1167322 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19710016314 |
| Archival Resource Key | ark:/13960/t1ck3534t |
| Language | English |
| Publisher Date | 1971-05-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |