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Drag and cooling with various forms of cowling for a whirlwind engine in a cabin fuselage
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1928 |
| Description | An investigation on the cowling of radial air-cooled engines was conducted in the 20-foot Propeller Research Tunnel at Langley Field. Cooling and drag tests were made with each form of cowling. The propulsive efficiency was found to be practically the same with all forms of cowling. |
| File Size | 22336032 |
| Page Count | 46 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081085 |
| Archival Resource Key | ark:/13960/t9z069q1v |
| Language | English |
| Publisher Date | 1928-01-01 |
| Access Restriction | Open |
| Subject Keyword | 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 |