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Scale-effect tests in a turbulent tunnel of the naca 65(sub 3)-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1944 |
| File Size | 857815 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092796 |
| Archival Resource Key | ark:/13960/t0sr23c7t |
| Language | English |
| Publisher Date | 1944-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils-naca 653-418-char , Moments & Ordinates Low-drag-(wing Flaps, Split) Scale Effect-airfoils-naca 653-418 Wing Flaps, Split Reynolds Number 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 |