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Full-scale tunnel investigation of the control and stability of a twin-engine monoplane with propellers operating
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1942 |
| File Size | 37630769 |
| Page Count | 111 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092514 |
| Archival Resource Key | ark:/13960/t0jt2vp41 |
| Language | English |
| Publisher Date | 1942-01-01 |
| Access Restriction | Open |
| Subject Keyword | Lift, Drag & Pitching Moments - Monoplanes Elevators - Efficiency Propellers, Tractor Air Flow - Tail Surfaces Downwash Angles Wing Flaps - Deflection Stabilizers Stability - Monoplanes Propeller Slipstream - Effect On Lift Tail Surfaces, Horizontal - Wind Tunnel Tests 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 |