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Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an naca 65(sub 1)-210 airfoil section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1945 |
| File Size | 41506019 |
| Page Count | 57 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092790 |
| Archival Resource Key | ark:/13960/t5z64vk3v |
| Language | English |
| Publisher Date | 1945-01-01 |
| Access Restriction | Open |
| Subject Keyword | Ailerons, Balanced - Sealed-gap Ailerons, Sealed-gap Airfoils - Naca 651-210 - Char , Moments & Ordinates - Low-drag Ailerons, Balanced - Internal Wind Tunnel Tests - Naca - Pressure, Low-turbulence (7 1/2' X 3') Airfoils Surfaces - Roughness Ailerons - Hinge Moments 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 |