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Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hanson, P. W. |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1957 |
| File Size | 9623210 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19710065201 |
| Archival Resource Key | ark:/13960/t5z617c61 |
| Language | English |
| Publisher Date | 1957-10-16 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Configurations Aspect Ratio Wings Lift Drag Ratio Subsonic Speed Wind Tunnel Stability Tests Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |