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Effects of wing-crank, leading-edge chord extensions and horizontal-tail height on the longitudinal stability of sweptwing models at mach numbers from 0.6 to 1.4
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1959 |
| Description | Effects of wing-crank, leading-edge chord extensions & horizontal-tail height on longitudinal stability of swept-wing models |
| File Size | 4420480 |
| Page Count | 117 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630003104 |
| Archival Resource Key | ark:/13960/t61599v8p |
| Language | English |
| Publisher Date | 1959-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamic Stability Tail Leading Edge Swept Wing Wing Planform 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 |