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Effects of compressibility on the flow past thick airfoil sections (Document No: 19930082274)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 15329811 |
| Page Count | 43 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082274 |
| Archival Resource Key | ark:/13960/t7np6d96p |
| Language | English |
| Publisher Date | 1948-07-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Naca - Characteristics Effect OF Compressibility Airfoils - Naca 0040-64 - Characteristics Airfoils - Naca 16-025 - Characteristics Airfoils - Naca 0040-65 - Characteristics Airfoils, Symmetrical - Characteristics Wind Tunnel Tests (naca- High-speed-18"x Airfoils - Naca 16-015 - Characteristics Airfoils - Naca 16-040 - Characteristics Airfoils - Thickness Airfoils - Naca 0040-63 - Characteristics 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 |