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Effect of leading-edge-flap deflection on the wing loads, load distributions, and flap hinge moments of the douglas x-3 research airplane at transonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1958 |
| File Size | 35402108 |
| Page Count | 88 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930090188 |
| Archival Resource Key | ark:/13960/t6qz6zm8d |
| Language | English |
| Publisher Date | 1958-07-15 |
| Access Restriction | Open |
| Subject Keyword | 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 |