Flight Test Results of a Subscale Super-STOL Aircraft
This paper presents the results from initial flight tests of a 30% scale demonstrator of a blown-wing SuperSTOL concept aircraft, intended for operation from extremely short runways of 100 ft or less. The subscale demonstrator is aimed at investigating the maximum achievable in-flight lift coefficie...
| Main Authors: | , , |
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| Other Authors: | |
| Format: | Article |
| Language: | English |
| Published: |
American Institute of Aeronautics and Astronautics
2021
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| Online Access: | https://hdl.handle.net/1721.1/130556 |