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Effects of reynolds number and leading-edge roughness on lift and drag characteristics of the naca 653-418, a=1.0 airfoil section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1945 |
| File Size | 7845044 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092798 |
| Archival Resource Key | ark:/13960/t3cz7jk7z |
| Language | English |
| Publisher Date | 1945-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnel Tests-naca-low-turbulence (lmal) Wind Tunnel Tests-naca-pressure, Two-dimensional(lmal) (7 1/2' X 3') Reynolds Number Airfoils-characteristics Effect OF Surface Roughness Airfoils-naca 653-418-low-drag Characteristics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |