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Test of naca 66,2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the xp-63 airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1942 |
| File Size | 1056979 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092767 |
| Archival Resource Key | ark:/13960/t19k7j99c |
| Language | English |
| Publisher Date | 1942-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wing Flaps, Slotted Wing Flaps, Balanced Pressure Distribution - Wing Flaps Airfoils - Naca 66,2-116 - Char & Moments Low-drag (wing Flaps, Balanced & Slot Wind Tunnel Tests - Naca - Pressure, Low-turbulence (7 1/2' X 3') Wings - Bell P-63 Wind Tunnel Tests (naca - 2-dim Pressure) Wing Flaps - 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 |