A fluidic thrust vector control using the bypass flow in a dual throat nozzle
Crossref DOI link: https://doi.org/10.1007/s12206-021-0716-8
Published Online: 2021-07-22
Published Print: 2021-08
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Wu, Kexin
Kim, HeuyDong
Text and Data Mining valid from 2021-07-22
Version of Record valid from 2021-07-22
Article History
Received: 3 November 2020
Revised: 29 March 2021
Accepted: 19 May 2021
First Online: 22 July 2021