A propeller design and analysis capability evaluation for high altitude application
The purpose of this research is the evaluation of a relatively simple minimum induced loss propeller design and a radially-graded momentum theory analysis method to provide the initial propeller design and analysis capability for predicting propeller performance of a High Altitude Long Endurance...
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| Format: | Others |
| Language: | en |
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2011
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| Online Access: | http://hdl.handle.net/10539/9488 |