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Design and evaluation of an integrated quiet, clean general aviation turbofan (qcgat) engine and aircraft propulsion system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wilson, C. German, J. Fogel, P. |
| Copyright Year | 1980 |
| Description | The design was based on the LTS-101 engine family for the core engine. A high bypass fan design (BPR=9.4) was incorporated to provide reduced fuel consumption for the design mission. All acoustic and pollutant emissions goals were achieved. A discussion of the preliminary design of a business jet suitable for the developed propulsion system is included. It is concluded that large engine technology can be successfully applied to small turbofans, and noise or pollutant levels need not be constraints for the design of future small general aviation turbofan engines. |
| File Size | 10243061 |
| Page Count | 238 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810023604 |
| Archival Resource Key | ark:/13960/t58d4qn3z |
| Language | English |
| Publisher Date | 1980-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Evaluation Civil Aviation Engine Design Engine Noise Jet Aircraft Noise Noise Reduction Quiet Engine Program Turbofan Engines General Aviation 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 |
