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Boundary-layer and stalling characteristics of the naca 64a006 airfoil section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 13148237 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082600 |
| Archival Resource Key | ark:/13960/t3gx8nc60 |
| Language | English |
| Publisher Date | 1949-08-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnel Tests - Aal (10'x7',no 1) Airfoils - Naca 64a006 - Char & Moments Low-drag Pressure Distribution - Airfoils - Naca 64a006 Boundary Layer Control - Airfoils - Naca 64a006 Air Flow - Visualization Air Flow - Airfoils Stalling 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 |