Aerodynamic Design of the NASA Rotor 67 for Non Uniform Inflow Due to Boundary Layer Ingestion
As the demand to improve the fuel efficiency of current commercial aircraft increases, new commercial airliner concepts such as the Blended Wing Body has been researched on and studied in various aspects over the years as an efficient alternative to the conventional transport configuration. One part...
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| Format: | Others |
| Language: | English |
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KTH, Kraft- och värmeteknologi
2015
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-180446 |