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Propulsion technology for an advanced subsonic transport
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Beheim, M. A. Antl, R. J. Povolny, J. H. |
| Copyright Year | 1972 |
| Description | Engine design studies for future subsonic commercial transport aircraft were conducted in parallel with airframe studies. These studies surveyed a broad distribution of design variables, including aircraft configuration, payload, range, and speed, with particular emphasis on reducing noise and exhaust emissions without severe economic and performance penalties. The results indicated that an engine for an advanced transport would be similar to the currently emerging turbofan engines. Application of current technology in the areas of noise suppression and combustors imposed severe performance and economic penalties. |
| File Size | 3333246 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720023128 |
| Archival Resource Key | ark:/13960/t75t8d804 |
| Language | English |
| Publisher Date | 1972-09-01 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Turbofan Engines Engine Design Transport Aircraft Noise Reduction Subsonic Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
