Numerical simulation of the unsteady combustion of solid rocket propellants at a harmonic pressure change
Crossref DOI link: https://doi.org/10.1007/s12206-019-1246-5
Published Online: 2020-01-10
Published Print: 2020-01
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Alexey, Krainov
Vasiliy, Poryazov
Dmitry, Krainov
Text and Data Mining valid from 2020-01-01
Version of Record valid from 2020-01-01
Article History
Received: 12 July 2019
Revised: 8 October 2019
Accepted: 15 October 2019
First Online: 10 January 2020