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Use of experimental steady-flow aerodynamic parameters in the calculation of flutter characteristics for finite-span swept on unswept wings at subsonic, transonic, and supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1960 |
| Description | Aerodynamic load and flutter on swept and unswept wings at various speeds |
| File Size | 23019330 |
| Page Count | 53 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630004021 |
| Archival Resource Key | ark:/13960/t25b4tz3s |
| Language | English |
| Publisher Date | 1960-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamic Load Swept Wing Unswept Wing 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 |