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Effect of centrifugal force on critical flutter speed on a uniform cantilever beam
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| Description | Semirigid flutter theory is used. Calculations are made on airfoils with fundamental bending frequencies up to 2000 radian per second. Centrifugal force can under certain conditions reduce the critical flutter speed. |
| File Size | 1058259 |
| Page Count | 19 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085561 |
| Archival Resource Key | ark:/13960/t03z2kz2p |
| Language | English |
| Publisher Date | 1948-06-18 |
| Access Restriction | Open |
| Subject Keyword | Vibration AND Flutter Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |