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The characteristics of the naca m-12 airfoil section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1926 |
| Description | The data obtained on the NACA M-12 airfoil, tested at twenty atmosphere density in the NACA variable density wind tunnel, have been extended by additional tests at one and at twenty atmospheres under improved conditions. The results of these tests are given. Considerable scale effect was found. |
| File Size | 370799 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081048 |
| Archival Resource Key | ark:/13960/t9477k825 |
| Language | English |
| Publisher Date | 1926-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Clark Y - Char & C P Airfoils - Angle OF Attack Airfoils, N A C A - M6 Char & C P Airfoils - Naca 997 - Characteristics Airfoils - 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 |