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Effects of nacelle position on wing-nacelle interference
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 38845986 |
| Page Count | 88 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082243 |
| Archival Resource Key | ark:/13960/t6rz3m32t |
| Language | English |
| Publisher Date | 1948-06-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Distribution - Wings Fuselages - Naca 111 (mod ) Pressure Distribution - Engine Nacelles Wind Tunnel Tests (naca-0-high-speed (16')) Wind Tunnel Tests - Naca - High-speed (16') Work Carried On At Lmal Nacelle - Wing Combinations Interference - Nacelles & Wings Airfoils - Naca 65-210 (mod ) - Char & Ordinates Low-drag 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 |