Loading...
Please wait, while we are loading the content...
Similar Documents
Longitudinal stability characteristics of a 42 degree sweptback wing and tail combination at a reynolds number of 6.8 x 10(exp 6)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| Description | Results are given of a wind-tunnel investigation at a Reynolds number of 6.8 x 10(exp 6) to determine the static longitudinal stability characteristics of a 42 degree sweptback wing and fuselage combination with a sweptback horizontal tail. Included are the effects of vertical position of fuselage and tail with respect to wing for several combinations of high-lift and staff-control devices. Also included is the effect of a simulated ground. |
| File Size | 20086273 |
| Page Count | 46 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085375 |
| Archival Resource Key | ark:/13960/t6547213r |
| Language | English |
| Publisher Date | 1948-07-22 |
| Access Restriction | Open |
| Subject Keyword | Flaps - Complete Wings Tail-wing AND Fuselage Combinations - Airplanes Stability, Longitudinal - Static Slots AND Slats - Complete Wings Wing-fuselage Combination - Airplanes Wake - Complete Wings 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 |