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An evaluation of the characteristics of a 10-percent-thick naca 66-series airfoil section with a special mean-camber line designed to produce a high critical mach number
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 9458560 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082303 |
| Archival Resource Key | ark:/13960/t2f80pp1v |
| Language | English |
| Publisher Date | 1948-07-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Characteristics - Effect OF Surface Roughness Airfoils - Naca 66(09)-210(1=1 0,c1i=0 6) - Char , Moments & Ordinates (a=0 6,c1 Airfoils - Naca 66-210 - Char & Moments Low-drag (wing Flaps,split) Pressure D Airfoils - Naca 66-210 (a=1 0,c1i=0 6) - Char , Moments & Ordinates (09) (a=0 6, 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 |