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| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1942 |
| Description | At the request of the Army Air Forces, Materiel Command, tests were made in the two-Dimensional low-turbulence tunnel of a mode l submitted by Bell Aircraft Corporation as the tip section of the wing of the xp-63 airplane. " The model was a NACA 66, 2x-2l6 a = 0.6 airfoil section of 50-inch chord and made of dural according to standard sheet-metal practice. The model was fitted for an internal-balance aileron with a tab and a Frise type aileron. Several alterations of the skirts and balance on the internal- balance aileron were tested to obtain the various aerodynamic characteristics of the aileron. |
| File Size | 14839144 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092768 |
| Archival Resource Key | ark:/13960/t0vq64q61 |
| Language | English |
| Publisher Date | 1942-01-01 |
| Access Restriction | Open |
| Subject Keyword | Ailerons - Deflection Ailerons - Bristol Frise Wind Tunnel Tests-naca-pressure, Low-turbulence (7 1/2' X 3') Airfoils - Naca 66,2x-216 - Char & Moments Low-drag Airfoils - Naca 66,2x-116 - Char & Moments Low-drag Ailerons, Balanced Wings - Bell P-63 Wind Tunnel Tests (naca - Low-turbulence & 2-dim Press ) Tabs, Aileron 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 |