Calculation of the unsteady burning velocity according to a known law of pressure variation during transient processes in a solid-propellant rocket engine
Crossref DOI link: https://doi.org/10.1134/S1990793114030099
Published Online: 2014-07-06
Published Print: 2014-05
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Marshakov, V. N.
Puchkov, V. M.
Text and Data Mining valid from 2014-05-01
