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Wind-tunnel investigation of an naca 23012 airfoil with an 18.05 percent chord maxwell slat and with trailing-edge flaps
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1941 |
| File Size | 2875721 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092829 |
| Archival Resource Key | ark:/13960/t9n33261b |
| Language | English |
| Publisher Date | 1941-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wing Flaps, Split - Full-span (20%-chord) Wing Slots, Maxwell & Flaps, Slotted & Split Wing Slats & Flaps, Slotted & Split Airfoils - Naca 23012 - Char Moments & Ordinates Wing Slots - Maxwell Wing Flaps, Slotted - Full-span (25 66%-chord) Wing Slots - Effect OF Gap 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 |