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Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings incorporating leading edge camber as influenced by reynolds numbers up to 8.00 x 10(exp 6) and mach numbers up to 0.29
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1955 |
| File Size | 2200202 |
| Page Count | 45 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930088997 |
| Archival Resource Key | ark:/13960/t8tb5v07h |
| Language | English |
| Publisher Date | 1955-10-06 |
| 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 |