Thrust Augmentation by Airframe-Integrated Linear-Spike Nozzle Concept for High-Speed Aircraft

Author： Takahashi Hidemi   Munakata Toshihiko   Sato Shigeru  

Publisher： MDPI

E-ISSN： 2226-4310|5|1|19-19

ISSN： 2226-4310

Source： Aerospace, Vol.5, Iss.1, 2018-02, pp. : 19-19

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