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Effects of a typical nacelle on the characteristics of a thick low-drag airfoil critically affected by leading-edge roughness
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1943 |
| File Size | 396658 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930093295 |
| Archival Resource Key | ark:/13960/t9186hm0w |
| Language | English |
| Publisher Date | 1943-01-01 |
| Access Restriction | Open |
| Subject Keyword | Engine Nacelles Airfoil Surfaces-roughness Airfoils, Low-drag-thick - Effect OF Leading Edge Roughness Wind Tunnel Tests-naca-pressure, Low-turbulance (7 1/2' X 3') Airfoils-naca 65,2-422 (approx )-characteristics Low-drag Interference-nacelles & Wings 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 |