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Boundary-layer and stalling characteristics of the naca 63-009 airfoil section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 14765156 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082575 |
| Archival Resource Key | ark:/13960/t2895j750 |
| Language | English |
| Publisher Date | 1949-06-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Distribution - Airfoils - Naca 63-009 Wind Tunnel Tests - Aal (10'x7'),( No 1) Air Flow - Visualization Air Flow - Airfoils Boundary Layer Control - Airfoils - Naca 63-009 Stalling Airfoils - Naca 63-009 - Char & Ordinates - Low-drag 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 |