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摘要: 开展2组先进钻地缩比弹高速侵彻混凝土实验,侵彻速度在1130~1650m/s之间。针对弹体结 构特点,金相分析了侵彻后剩余弹体,发现弹体与靶接触的表面(包括弹头和壳体段)均存在明显热影响区 (Heataffectedzone,HAZ),而与靶脱离接触部分未发现明显热影响区,因而弹靶相互作用是热影响区产生的 主要原因。在弹尖部位存在少量绝热剪切带(Adiabaticshearingband,ASB),其对弹体质量损失有一定贡献, 但在实验撞击速度范围内其影响有限。ASB可能引起弹尖非对称磨蚀,进而降低弹体侵彻性能。Abstract: Inordertoenhancethestructuralstabilityofearthpenetrationwarhead (EPW)inhighspeedpenetration, theadvancedEPW wasdesigned.Theperformanceofthereduced-scaleadvanced EPW wasexperimentallystudiedduringthestrikingvelocitybetween1130~1650m/s.Theresidual projectileswerestudiedbymetallography.Itisfoundthattheheataffectedzone(HAZ)isdistributed aroundtheprojectilesurfacewheretheprojectileandtargetcontact,includingtheprojectilenoseand shank.ThereisnosignificantHAZintheareawheretheprojectileandtargetoffcontact.ItisconcludedthattheinteractionbetweentargetandprojectilebringsHAZin. Ontheotherhand,thereare severaladiabaticshearingbands(ASBs)distributedattheprojectilenosetip.AlthoughASBhaspositivecontributiontotheprojectilemassloss, theinfluencecanbeneglectedduringtheexperimental strikingvelocityrangeduetotherarenumberofASBandthelimiteddistributionarea.However, ASBmayleadtothenonsymmetricalabrasionofpenetratorandthendecreasetheperformanceofprojectileathigherpenetrationvelocity.
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