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Drag analysis of single-engine military airplanes tested in the naca full-scale wind tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1940 |
| File Size | 49591824 |
| Page Count | 88 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092657 |
| Archival Resource Key | ark:/13960/t6545x34q |
| Language | English |
| Publisher Date | 1940-01-01 |
| Access Restriction | Open |
| Subject Keyword | Radiators - Cooling Radio Antennas - Drag Cockpit Tops Drag-wings-effect OF Surface Roughness Propeller Blade Cuffs AND Spinners Meredith Effect Exhaust Stacks Landing Gears, Retractable - Drag-wind Tunnel Tests - (naca-full- Scale) Windshields - Drag - Wind Tunnel Tests (naca-full-scale) 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 |