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- W2349753282 abstract "Based on the fast change of pressure in closed bomb tests,a heat flux equation focused on pressure factor was deducted.A one-dimensional semi-infinite model of calculating inwall heat transfer in closed bomb tests was established and the expression of heat transfer was obtained.The model was validated by double base aromatic-3(SF-3),TEGDN(TG) propellant and triple-base propellant.The results show that the error between corrected whole heat loss and theoretical whole heat loss is less than 10%,and the burning rate pressure index of SF-3 propellant obtained is close to the expected value." @default.
- W2349753282 created "2016-06-24" @default.
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- W2349753282 date "2009-01-01" @default.
- W2349753282 modified "2023-09-24" @default.
- W2349753282 title "Heat Loss Correction in Closed Bomb Tests" @default.
- W2349753282 hasPublicationYear "2009" @default.
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