Performance Calculation and Design of Stratospheric Propeller
A new high altitude propeller is analyzed and designed in this paper to be used on the stratospheric aircraft propulsion system. Two more appropriate approaches to investigate the aerodynamics characteristics of the high altitude propeller are obtained by comparison of vortex theory with the Spalart...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
IEEE
2017-01-01
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| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/7982612/ |