Experimental results for 25-mm and 51-mm rotating detonation rocket engine combustors
Crossref DOI link: https://doi.org/10.1007/s00193-023-01120-x
Published Online: 2023-04-12
Published Print: 2023-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Knowlen, C. http://orcid.org/0000-0003-3389-8497
Mundt, T.
Kurosaka, M.
Funding for this research was provided by:
Air Force Office of Scientific Research (FA 9550-18-1-9-0076)
Text and Data Mining valid from 2023-04-01
Version of Record valid from 2023-04-01
Article History
Received: 22 November 2022
Accepted: 11 February 2023
First Online: 12 April 2023