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: | Courtin, Christopher, Hansman Jr, Robert J, Drela, Mark |
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Other Authors: | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics |
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 |
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