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Some lift and drag measurements of two configurations of a nacelle and oil-cooler scoop for the hughes-kaiser cargo airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1943 |
| File Size | 8752616 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930093297 |
| Archival Resource Key | ark:/13960/t7qn9bn96 |
| Language | English |
| Publisher Date | 1943-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnel Tests (naca - Pressure, Low-turbulence) Seaplanes, Cargo Scoops Airfoils - Naca 63,4-41(20 2) (approx ) Low-drag Engine Nacelles - Kaiser-hughes Wind Tunnel Tests - Naca - Pressure, Low-turbulence (7 1/2' X 3') Seaplanes - Kaiser-hughes Airfoils - Naca 23021 Wind Tunnel Tests (naca - 2-dim Pressure) (amer ) Nacelle-wing Combinations 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 |