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Review of aircraft engine fan noise reduction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | VanZante, Dale |
| Copyright Year | 2008 |
| Description | Aircraft turbofan engines incorporate multiple technologies to enhance performance and durability while reducing noise emissions. Both careful aerodynamic design of the fan and proper installation of the fan into the system are requirements for achieving the performance and acoustic objectives. The design and installation characteristics of high performance aircraft engine fans will be discussed along with some lessons learned that may be applicable to spaceflight fan applications. |
| File Size | 1492213 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080047681 |
| Archival Resource Key | ark:/13960/t37131v0w |
| Language | English |
| Publisher Date | 2008-04-02 |
| Access Restriction | Open |
| Subject Keyword | Acoustics Lessons Learned Engine Noise Noise Reduction Aerodynamic Noise Durability Aerodynamics Turbofan Engines Space Flight Fighter Aircraft Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |