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Optimization of structures to satisfy aeroelastic requirements
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rudisill, C. S. |
| Copyright Year | 1975 |
| Description | A method for the optimization of structures to satisfy flutter velocity constraints is presented along with a method for determining the flutter velocity. A method for the optimization of structures to satisfy divergence velocity constraints is included. |
| File Size | 521998 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750007567 |
| Archival Resource Key | ark:/13960/t15n10d0x |
| Language | English |
| Publisher Date | 1975-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Weight Mass Structural Stability Structural Vibration Lift Devices Structural Design Criteria Flutter Analysis Aeroelasticity Optimization 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 |