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High-speed tests of an airfoil section cambered to have critical mach numbers higher than those attainable with a uniform-load mean line
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1947 |
| File Size | 13537973 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082040 |
| Archival Resource Key | ark:/13960/t3xt01x56 |
| Language | English |
| Publisher Date | 1947-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Characteristics - Effect OF Compressibility Work Carried On At Aal Pressure Distribution - Airfoils - Naca 66(109)-210 Ordinates - Low-drag Airfoils - Naca 66-210 - Char & Moments - Low-drag Airfoils - Naca 66(109)-210 (a=1 0,cli=0 6)- Char ,moments & (a=0 6,cli=-0 4) Wind Tunnel Tests - Aal - High-speed (3 1/2'x1') Airfoils, Cambered - Characteristics - Wind Tunnel Tests 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 |