Volume 32 Issue 3
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LI Xiao-jie, ZHAO Chun-feng. Characteristiccurvemethodforanalyzingmovementofflyerplatebasedonuniversalequationofstateofexplosive[J]. Explosion And Shock Waves, 2012, 32(3): 237-242. doi: 10.11883/1001-1455(2012)03-0237-06
Citation: LI Xiao-jie, ZHAO Chun-feng. Characteristiccurvemethodforanalyzingmovementofflyerplate basedonuniversalequationofstateofexplosive[J]. Explosion And Shock Waves, 2012, 32(3): 237-242. doi: 10.11883/1001-1455(2012)03-0237-06

Characteristiccurvemethodforanalyzingmovementofflyerplate basedonuniversalequationofstateofexplosive

doi: 10.11883/1001-1455(2012)03-0237-06
Funds:

NationalNaturalScienceFoundationofChina(10972051)

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  • Corresponding author: ZHAO Chun-feng
  • Publish Date: 2012-05-25
  • Fromthephysicaldefinitionofperturbationpropagation(Machwaves),thecharacteristic equationsofatwo-dimensionalsupersonicflowwerededucedintotheformswhichwereuncorrelated withtheformulaofEOS.Meanwhile,anewPrantl-Meyerfunctionwasexpressedintoasimplevariablefunctionoffluiddensityalso. Basedoncharacteristicdifference,asolutionmethodofthetwo-dimensionalsupersonicflowwasbuiltup. Therefore,asanapplicationexampleofthesolutionmethod, themovementoftheflyerplatedrivenbyglancingdetonationwasanalyzed.Forcomparison,DetonationdrivesoftheTNTandemulsionexplosiveswerecalculatedwithJWLandpolytropicEOSs. The numericalresultsshowthatcharacteristicdifferencesolutionscompletelyagreewiththeexpanding worksofexplosiveEOSs.
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