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Control vane for engine exhaust flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Shaw, C. S. Wilson, J. C. |
| Copyright Year | 1974 |
| Description | Vane solves problem of hot-gas exhaust impingement on curved-duct exteriors, shielding, and other nearby structure components. To eliminate secondary egress of exhaust, curved vane is placed upstream of engine exhaust duct and in close proximity to exhaust exit to induce free-stream flow more in line with exit. |
| File Size | 97148 |
| Page Count | 2 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740000138 |
| Archival Resource Key | ark:/13960/t3518s25c |
| Language | English |
| Publisher Date | 1974-09-01 |
| Access Restriction | Open |
| Subject Keyword | Thermal Protection Engine Design Gas Flow Control Surfaces Vanes Secondary Flow Helicopter Design Exhaust Systems 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 |