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Free-flight-tunnel investigation of the effect of mode of propeller rotation uuon the lateral-stability characteristics of a twin-engine airplane model with single vertical tails of different size
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1943 |
| File Size | 15178924 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092563 |
| Archival Resource Key | ark:/13960/t52g0z05m |
| Language | English |
| Publisher Date | 1943-01-01 |
| Access Restriction | Open |
| Subject Keyword | Instability, Spiral Wing Flaps, Slotted-partial-span Propellers - Rotation Propeller Slipstream - Effect On Stability Wing Flaps - Deflection Tail Surfaces, Vertical-two-engine Airplanes Airplanes, Two-engine Airplanes, Bombing - Wind Tunnel Tests Air Flow - Tail Surfaces Stability & Control, Lateral Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |