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Wind-tunnel investigation of the naca 654-421 airfoil section with a double slotted flap and boundary layer control by suction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1947 |
| File Size | 18098785 |
| Page Count | 33 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082039 |
| Archival Resource Key | ark:/13960/t1pg61018 |
| Language | English |
| Publisher Date | 1947-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnel Tests - Naca - Low-turbulence (7 1/2'x 3') Work Carried On At Lmal Wing Flaps, Slotted - Double Boundary Layer Control - Airfoils - Naca 654-421 Airfoils - Characteristics Effect OF Surface Roughness Slotted (double)) Boundary Layer Control - Suction - Slots Airfoils - Naca 654-421 - Char & Ordinates Low-drag(wing Flaps, 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 |