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Energy efficient engine: preliminary design and integration studies
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gray, D. E. |
| Copyright Year | 1978 |
| Description | A mixed exhaust, direct drive fan turbofan configuration was selected from four candidates. This choice was based on its ability to exceed study goals of 12% lower thrust specific fuel consumption and 5% lower direct operating cost by the 1990's with commercially acceptable technical risk and relative mechanical simplicity. The evaluation leading to configuration selection is discussed. Necessary technology advancements are identified and related to the goals. |
| File Size | 1433617 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780019110 |
| Archival Resource Key | ark:/13960/t6m08x49c |
| Language | English |
| Publisher Date | 1978-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Engine Design Energy Conservation Transport Aircraft Fuel Consumption Turbofan Engines Commercial Aircraft Aircraft Engines Propulsion System Configurations Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |