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Wind-tunnel tests of ailerons at various speeds ii : ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the naca 66,2-216 airfoil
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1943 |
| File Size | 23306514 |
| Page Count | 65 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092930 |
| Archival Resource Key | ark:/13960/t3qv6r57r |
| Language | English |
| Publisher Date | 1943-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils-naca 66,2-216-char , Moments & Ordinates Low-drag Ailerons, Balanced - Hinge Moments Mach Number Ailerons, Balanced - Sealed-gap Pressure Distribution-airfoil-naca 66,2-216 Ailerons, Balanced - Internal Flying, High-speed Ailerons - Wind Tunnel Tests Control Sticks-forces Wind Tunnel Tests-naca-stability 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 |