Conceptual study of supersonic transports employing airframe-integrated advanced nozzle configuration
A conceptual study of a supersonic cruise aircraft employing an airframe-integrated linear aerospike propulsion system was conducted based on the evaluation of the thrust performance, propulsion efficiency, cruise performance, and flight attitude characteristics. The thrust performance was evaluated...
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| Format: | Article |
| Language: | English |
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The Japan Society of Mechanical Engineers
2017-12-01
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| Series: | Journal of Fluid Science and Technology |
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| Online Access: | https://www.jstage.jst.go.jp/article/jfst/12/3/12_2017jfst0026/_pdf/-char/en |