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A preliminary investigation of the characteristics of air scoops on a fuselage
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1942 |
| File Size | 8967323 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092958 |
| Archival Resource Key | ark:/13960/t8pc66778 |
| Language | English |
| Publisher Date | 1942-01-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Distribution - Fuselages Ducts Mach Number Boundary Layer Fuselages - Naca 111 - Wind Tunnel Tests (naca-prt) Scoops Airfoils - Naca 0015 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 |