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Wind-tunnel investigation of effect of yaw on lateral-stability characteristics v : symmetrically tapered wing with a circular fuselage having a horizontal and a vertical tail
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1943 |
| File Size | 1170200 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092567 |
| Archival Resource Key | ark:/13960/t3rv3s251 |
| Language | English |
| Publisher Date | 1943-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wing Flaps, Split - Partial-span (20%-chord) Tail Surfaces, Vertical Stability, Lateral Rolling & Yawing Moments - Airfoils - Naca 23012 Tail Surfaces - End Plates Tail Surfaces, Horizontal - Wind Tunnel Tests Fuselages, Circular Wings - Dihedral & Sweepback Wings, Tapered - Characteristics Effect OF Wing Flaps Wings - Stability, Lateral 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 |