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Wind-tunnel investigation of a high-critical-speed fuselage scoop including the effects of boundary layer
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1945 |
| File Size | 28399752 |
| Page Count | 77 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092959 |
| Archival Resource Key | ark:/13960/t2m65v18j |
| Language | English |
| Publisher Date | 1945-01-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Distribution - Fuselages Wind Tunnel Tests - Naca - High-speed (8') Boundary Layer Scoops Photography - Air Flow - Scoops - Tufts Mach Number 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 |