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Two-dimensional wind-tunnel investigation of spoiler aileron flap model for the hughes xf-11 airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1945 |
| File Size | 31075896 |
| Page Count | 73 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092940 |
| Archival Resource Key | ark:/13960/t0ps24175 |
| Language | English |
| Publisher Date | 1945-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wing Spoilers, Retractable Ailerons, Retractable Wing Flaps, Slotted & Ailerons, Retractable Wind Tunnel Tests - Naca - Pressure, Low-turbulence (7 1/2' X 3') Airfoils - Naca 66(215)-216 (approx ) - Char , Moments & Ordinates Low-drag (wing Flaps, Slotted) Wind Tunnel Tests - Naca - Low-turbulence (7 1/2' X 3') Ailerons - Hughes F-11 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 |