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彈性力學(xué)仿真軟件:LS-DYNA:LS-DYNA顯式動(dòng)力學(xué)模擬實(shí)踐1彈性力學(xué)仿真軟件:LS-DYNA顯式動(dòng)力學(xué)模擬實(shí)踐1.11LS-DYNA軟件概述LS-DYNA是一款廣泛應(yīng)用于汽車、航空航天、國(guó)防、土木工程等領(lǐng)域的高級(jí)非線性動(dòng)力學(xué)有限元分析軟件。它由LivermoreSoftwareTechnologyCorporation(LSTC)開(kāi)發(fā),能夠處理復(fù)雜的顯式和隱式動(dòng)力學(xué)問(wèn)題,包括碰撞、爆炸、高速?zèng)_擊等。LS-DYNA的核心優(yōu)勢(shì)在于其強(qiáng)大的求解器,能夠高效地模擬材料的非線性行為和大變形問(wèn)題。1.1.1主要功能顯式動(dòng)力學(xué)分析:適用于短時(shí)間、大變形的動(dòng)力學(xué)問(wèn)題,如碰撞、爆炸等。隱式動(dòng)力學(xué)分析:適用于長(zhǎng)時(shí)間、小變形的動(dòng)力學(xué)問(wèn)題,如結(jié)構(gòu)靜力分析。多物理場(chǎng)耦合分析:能夠模擬流固耦合、熱固耦合等多物理場(chǎng)問(wèn)題。材料模型:提供多種材料模型,包括金屬、復(fù)合材料、混凝土、橡膠等。接觸算法:支持多種接觸算法,如自動(dòng)接觸、自定義接觸等,用于處理復(fù)雜的接觸問(wèn)題。1.1.2應(yīng)用案例汽車碰撞模擬:LS-DYNA被廣泛用于汽車碰撞安全分析,預(yù)測(cè)碰撞時(shí)車輛的變形和乘員的傷害。爆炸效應(yīng)分析:在國(guó)防和安全領(lǐng)域,LS-DYNA用于模擬爆炸對(duì)結(jié)構(gòu)的影響,評(píng)估防護(hù)措施的有效性。土木工程應(yīng)用:在土木工程中,LS-DYNA用于地震響應(yīng)分析,預(yù)測(cè)建筑物在地震中的行為。1.22顯式動(dòng)力學(xué)模擬基礎(chǔ)顯式動(dòng)力學(xué)模擬是一種數(shù)值方法,用于解決動(dòng)力學(xué)問(wèn)題,特別是那些涉及短時(shí)間尺度和大變形的問(wèn)題。在LS-DYNA中,顯式動(dòng)力學(xué)模擬是通過(guò)時(shí)間步進(jìn)方法實(shí)現(xiàn)的,其中每個(gè)時(shí)間步長(zhǎng)內(nèi)的動(dòng)力學(xué)響應(yīng)是通過(guò)求解動(dòng)力學(xué)方程得到的。1.2.1基本原理顯式動(dòng)力學(xué)模擬基于牛頓第二定律,即力等于質(zhì)量乘以加速度。在有限元分析中,結(jié)構(gòu)被離散成多個(gè)單元,每個(gè)單元的運(yùn)動(dòng)狀態(tài)(位移、速度、加速度)通過(guò)時(shí)間步進(jìn)迭代計(jì)算。由于顯式方法不需要求解大型線性方程組,因此在處理大變形和非線性問(wèn)題時(shí)更為高效。1.2.2時(shí)間步長(zhǎng)選擇時(shí)間步長(zhǎng)的選擇對(duì)于顯式動(dòng)力學(xué)模擬至關(guān)重要。時(shí)間步長(zhǎng)必須足夠小,以確保模擬的穩(wěn)定性。通常,時(shí)間步長(zhǎng)由網(wǎng)格的最小尺寸和材料的波速?zèng)Q定,遵循CFL條件(Courant-Friedrichs-Lewy條件)。1.2.3材料模型在顯式動(dòng)力學(xué)模擬中,準(zhǔn)確的材料模型是關(guān)鍵。LS-DYNA提供了多種材料模型,包括但不限于:Johnson-Cook模型:適用于金屬材料在高溫和高速下的行為。Mohr-Coulomb模型:適用于土壤和巖石材料的模擬。Neo-Hookean模型:適用于橡膠和生物組織等超彈性材料。1.2.4接觸算法接觸算法用于處理不同物體之間的接觸和碰撞。LS-DYNA提供了多種接觸算法,包括:自動(dòng)接觸:軟件自動(dòng)識(shí)別接觸面,適用于簡(jiǎn)單接觸問(wèn)題。自定義接觸:用戶定義接觸面,適用于復(fù)雜接觸問(wèn)題。1.2.5示例:汽車碰撞模擬假設(shè)我們正在使用LS-DYNA進(jìn)行一個(gè)簡(jiǎn)單的汽車碰撞模擬。以下是一個(gè)簡(jiǎn)化版的輸入文件示例,用于設(shè)置模擬參數(shù)和模型:*KEYWORD

*CONTROL_TIMESTEP

0.0001,0.00001

*CONTROL_TERMINATION

1.0

*MATERIAL_ELASTIC

1,7850,210000,0.3

*PART

1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1

*NODE

1,0,0,0

2,1,0,0

3,1,1,0

4,0,1,0

*ELEMENT_SOLID

1,1,2,3,4

*INITIAL_VELOCITY

1,1,0,0,0

*END1.2.6解釋*CONTROL_TIMESTEP:設(shè)置時(shí)間步長(zhǎng)控制參數(shù),第一個(gè)值為初始時(shí)間步長(zhǎng),第二個(gè)值為最小時(shí)間步長(zhǎng)。*CONTROL_TERMINATION:設(shè)置模擬終止時(shí)間。*MATERIAL_ELASTIC:定義材料屬性,這里為彈性材料,密度為7850kg/m^3,楊氏模量為210000MPa,泊松比為0.3。*PART:定義零件,這里是一個(gè)簡(jiǎn)單的實(shí)體。*NODE:定義節(jié)點(diǎn)坐標(biāo)。*ELEMENT_SOLID:定義實(shí)體單元,這里是一個(gè)四節(jié)點(diǎn)四面體單元。*INITIAL_VELOCITY:設(shè)置初始速度,這里為零件1在x方向上的速度為1m/s。*END:輸入文件的結(jié)束標(biāo)記。通過(guò)這個(gè)簡(jiǎn)化的例子,我們可以看到LS-DYNA輸入文件的基本結(jié)構(gòu)和如何設(shè)置顯式動(dòng)力學(xué)模擬的參數(shù)。實(shí)際應(yīng)用中,模型會(huì)更加復(fù)雜,包括多個(gè)零件、復(fù)雜的材料模型和接觸條件。2安裝與配置2.1LS-DYNA安裝步驟在開(kāi)始安裝LS-DYNA之前,確保你的系統(tǒng)滿足軟件的最低硬件和軟件要求。LS-DYNA是一款高性能的有限元分析軟件,主要用于解決復(fù)雜的非線性動(dòng)力學(xué)問(wèn)題。下面的步驟將指導(dǎo)你完成LS-DNA的安裝過(guò)程:下載安裝包:訪問(wèn)LS-DYNA官方網(wǎng)站或通過(guò)授權(quán)的渠道獲取最新版本的安裝包。確保下載的版本與你的操作系統(tǒng)兼容。解壓安裝包:使用解壓縮軟件(如WinRAR或7-Zip)解壓下載的安裝包到一個(gè)指定的目錄。運(yùn)行安裝程序:找到解壓后的目錄中的安裝程序,通常是setup.exe或install.sh(對(duì)于Linux系統(tǒng)),雙擊運(yùn)行。接受許可協(xié)議:閱讀并接受LS-DYNA的許可協(xié)議。這是安裝過(guò)程中的必要步驟。選擇安裝類型:選擇“完整安裝”或“自定義安裝”。完整安裝會(huì)安裝所有組件,而自定義安裝允許你選擇特定的組件進(jìn)行安裝。指定安裝路徑:輸入你希望安裝LS-DYNA的路徑。建議選擇一個(gè)沒(méi)有中文或特殊字符的路徑,以避免潛在的安裝問(wèn)題。配置硬件鎖:如果你的許可證是基于硬件鎖的,確保在安裝過(guò)程中正確配置硬件鎖。這通常涉及到插入硬件鎖并按照提示進(jìn)行設(shè)置。安裝網(wǎng)絡(luò)許可證服務(wù)器:如果你計(jì)劃在多臺(tái)計(jì)算機(jī)上使用LS-DYNA,需要安裝網(wǎng)絡(luò)許可證服務(wù)器。這一步驟在安裝過(guò)程中可以選擇。完成安裝:點(diǎn)擊“完成”按鈕,等待安裝程序完成安裝過(guò)程。安裝完成后,重啟計(jì)算機(jī)以確保所有更改生效。2.2環(huán)境變量設(shè)置與檢查環(huán)境變量的正確設(shè)置對(duì)于LS-DYNA的運(yùn)行至關(guān)重要。下面是如何設(shè)置和檢查L(zhǎng)S-DYNA環(huán)境變量的步驟:2.2.1設(shè)置環(huán)境變量添加LS-DYNA路徑:將LS-DYNA的安裝路徑添加到系統(tǒng)環(huán)境變量PATH中。例如,如果你的LS-DYNA安裝在C:\LS-DYNA目錄下,你可以在PATH變量中添加C:\LS-DYNA\bin。設(shè)置許可證路徑:設(shè)置LS_DYNA_LICENSE_FILE環(huán)境變量,指向你的許可證文件或網(wǎng)絡(luò)許可證服務(wù)器的地址。例如,如果你的許可證文件位于C:\licenses\lsdyna.lic,則設(shè)置LS_DYNA_LICENSE_FILE=C:\licenses\lsdyna.lic。配置硬件鎖:如果使用硬件鎖,確保LS_DYNA_LICENSE_FILE指向硬件鎖的正確端口。例如,LS_DYNA_LICENSE_FILE=27000@hostname,其中hostname是運(yùn)行硬件鎖的計(jì)算機(jī)的名稱。2.2.2檢查環(huán)境變量在設(shè)置完環(huán)境變量后,可以通過(guò)以下步驟檢查它們是否正確設(shè)置:打開(kāi)命令行界面:在Windows上,打開(kāi)“命令提示符”;在Linux或Mac上,打開(kāi)“終端”。檢查PATH變量:輸入echo%PATH%(Windows)或echo$PATH(Linux/Mac),檢查L(zhǎng)S-DYNA的bin目錄是否在列表中。檢查L(zhǎng)S_DYNA_LICENSE_FILE變量:輸入echo%LS_DYNA_LICENSE_FILE%(Windows)或echo$LS_DYNA_LICENSE_FILE(Linux/Mac),確保輸出的路徑或地址與你的許可證設(shè)置相匹配。運(yùn)行測(cè)試程序:在命令行界面中運(yùn)行LS-DYNA的一個(gè)測(cè)試程序,如lsprepost或lsdyna,以驗(yàn)證環(huán)境變量是否正確設(shè)置。如果程序能夠成功運(yùn)行,說(shuō)明環(huán)境變量設(shè)置正確。2.2.3示例:在Linux下設(shè)置環(huán)境變量#在.bashrc文件中添加以下行

exportPATH=$PATH:/path/to/ls-dyna/bin

exportLS_DYNA_LICENSE_FILE=27000@licensing-server

#保存并關(guān)閉文件

#使更改生效

source~/.bashrc在上述示例中,我們首先在用戶的.bashrc文件中添加了PATH和LS_DYNA_LICENSE_FILE環(huán)境變量的設(shè)置。然后,通過(guò)運(yùn)行source~/.bashrc命令,使這些更改立即生效,無(wú)需重啟計(jì)算機(jī)。通過(guò)遵循上述步驟,你可以確保LS-DYNA在你的系統(tǒng)上正確安裝并配置,從而順利進(jìn)行顯式動(dòng)力學(xué)模擬實(shí)踐。3前處理基礎(chǔ)3.1幾何模型導(dǎo)入與編輯在進(jìn)行LS-DYNA顯式動(dòng)力學(xué)模擬前,幾何模型導(dǎo)入與編輯是至關(guān)重要的第一步。這一步驟確保了模擬的準(zhǔn)確性,因?yàn)槟P偷膸缀涡螤钪苯佑绊懥撕罄m(xù)的材料屬性分配、網(wǎng)格劃分以及邊界條件的設(shè)定。3.1.1導(dǎo)入幾何模型LS-DYNA支持多種格式的幾何模型導(dǎo)入,包括但不限于IGES、STEP、STL和CAD軟件的原生格式。例如,從SolidWorks導(dǎo)入模型時(shí),可以將模型保存為IGES格式,然后在LS-DYNA中使用*INCLUDE命令來(lái)讀取。*INCLUDE,IGES,"model.igs"3.1.2編輯幾何模型一旦模型導(dǎo)入,可能需要進(jìn)行一些編輯,如修復(fù)幾何缺陷、移除不必要的特征或合并實(shí)體。LS-DYNA提供了基本的幾何編輯工具,但更復(fù)雜的編輯通常在CAD軟件中完成,然后重新導(dǎo)入。3.1.2.1示例:修復(fù)模型假設(shè)模型中存在一些小的幾何缺陷,如縫隙或重疊面,可以使用*GEOM_FIX命令來(lái)嘗試自動(dòng)修復(fù)。*GEOM_FIX3.2材料屬性定義材料屬性定義是LS-DYNA模擬中的核心部分,它決定了模型在受力時(shí)的行為。LS-DYNA支持多種材料模型,包括彈性、塑性、復(fù)合材料等。3.2.1彈性材料對(duì)于彈性材料,通常需要定義楊氏模量(E)和泊松比(ν)。例如,定義一個(gè)彈性材料,其楊氏模量為200GPa,泊松比為0.3。*MAT_ELASTIC

1,0,200000,0.33.2.2塑性材料塑性材料的定義更為復(fù)雜,需要考慮屈服強(qiáng)度、硬化行為等。例如,定義一個(gè)塑性材料,使用Johnson-Cook模型。*MAT_PLASTIC_KINEMATIC

1,0,78000,0.3,0.0,1,1,1

*USERumat,"umat.f"在上述例子中,umat.f是一個(gè)Fortran子程序,用于定義Johnson-Cook材料模型的具體參數(shù)。3.3邊界條件與載荷設(shè)置邊界條件與載荷設(shè)置定義了模型在模擬過(guò)程中的外部環(huán)境,包括固定點(diǎn)、移動(dòng)邊界以及施加的力或壓力。3.3.1固定邊界條件固定邊界條件通常用于模擬模型的一部分被固定不動(dòng)的情況。例如,固定模型的底部。*BOUNDARY_SPC

1,1,1,1,1,1在上述命令中,1表示所有節(jié)點(diǎn),1,1,1,1,1,1分別表示固定x、y、z方向的位移和旋轉(zhuǎn)。3.3.2動(dòng)態(tài)載荷動(dòng)態(tài)載荷可以是力、壓力或加速度。例如,向模型的頂部施加一個(gè)1000N的力。*LOAD_CENTRIFUGAL

1,0,0,1000在上述命令中,1表示所有節(jié)點(diǎn),0,0,1000表示在z方向上施加1000N的力。3.3.3時(shí)間依賴載荷LS-DYNA支持時(shí)間依賴的載荷,這在模擬沖擊或爆炸等瞬態(tài)事件時(shí)非常有用。例如,使用*DEFINE_CURVE定義一個(gè)時(shí)間-力曲線,然后通過(guò)*LOAD_CURVE應(yīng)用。*DEFINE_CURVE

1,0,100,1000,200,0

*LOAD_CURVE

1,1在上述例子中,*DEFINE_CURVE定義了一個(gè)在100ms時(shí)達(dá)到1000N,然后在200ms時(shí)降為0的力曲線。*LOAD_CURVE則將這個(gè)曲線應(yīng)用到之前定義的載荷上。通過(guò)這些步驟,可以為L(zhǎng)S-DYNA顯式動(dòng)力學(xué)模擬準(zhǔn)備一個(gè)詳細(xì)的前處理模型,確保模擬結(jié)果的準(zhǔn)確性和可靠性。4顯式動(dòng)力學(xué)模擬設(shè)置4.1時(shí)間步長(zhǎng)控制4.1.1原理在LS-DYNA的顯式動(dòng)力學(xué)模擬中,時(shí)間步長(zhǎng)的控制至關(guān)重要。由于顯式算法的穩(wěn)定性條件,時(shí)間步長(zhǎng)通常由最短波長(zhǎng)和材料的波速?zèng)Q定,遵循CFL條件(Courant-Friedrichs-Lewy條件)。時(shí)間步長(zhǎng)過(guò)小會(huì)增加計(jì)算成本,而過(guò)大則可能導(dǎo)致模擬不穩(wěn)定。4.1.2內(nèi)容LS-DYNA通過(guò)關(guān)鍵字*CONTROL_TIMESTEP來(lái)控制時(shí)間步長(zhǎng)。此關(guān)鍵字允許用戶設(shè)定最小和最大時(shí)間步長(zhǎng),以及時(shí)間步長(zhǎng)的調(diào)整策略。4.1.2.1示例代碼*CONTROL_TIMESTEP

0.0,0.0001,0.001,0.00001,0.000001,0.0000001,0.00000001,0.000000001,0.0000000001,0.00000000001解釋:第一個(gè)參數(shù)(0.0)表示不使用用戶定義的時(shí)間步長(zhǎng)。第二個(gè)參數(shù)(0.0001)是時(shí)間步長(zhǎng)的最小值。第三個(gè)參數(shù)(0.001)是時(shí)間步長(zhǎng)的最大值。其余參數(shù)用于控制時(shí)間步長(zhǎng)的調(diào)整策略,如時(shí)間步長(zhǎng)的最小變化率、最大變化率等。4.2接觸算法選擇與配置4.2.1原理接觸算法在LS-DYNA中用于處理不同物體之間的接觸和碰撞。顯式動(dòng)力學(xué)模擬中,接觸算法的選擇和配置直接影響模擬的準(zhǔn)確性和效率。LS-DYNA提供了多種接觸算法,包括表面-表面接觸、節(jié)點(diǎn)-表面接觸等。4.2.2內(nèi)容接觸算法的配置通過(guò)關(guān)鍵字*CONTACT系列來(lái)實(shí)現(xiàn)。例如,*CONTACT_SURFACE_TO_SURFACE用于定義表面-表面接觸。4.2.2.1示例代碼*CONTACT_SURFACE_TO_SURFACE

1,1,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,

#案例分析

##subdir5.1碰撞模擬案例

###碰撞模擬原理

碰撞模擬在LS-DYNA中是一個(gè)關(guān)鍵應(yīng)用領(lǐng)域,主要用于汽車、航空航天、軍事和工業(yè)設(shè)計(jì)等行業(yè)。顯式動(dòng)力學(xué)模擬允許用戶精確地模擬高速碰撞事件,如汽車碰撞測(cè)試、飛行器著陸沖擊等。LS-DYNA通過(guò)求解牛頓第二定律的微分方程,跟蹤材料在碰撞過(guò)程中的變形和應(yīng)力變化,從而預(yù)測(cè)結(jié)構(gòu)的響應(yīng)和可能的損壞。

###碰撞模擬內(nèi)容

在碰撞模擬中,LS-DYNA使用有限元方法(FEM)來(lái)離散結(jié)構(gòu),將結(jié)構(gòu)分解為許多小的單元,每個(gè)單元的運(yùn)動(dòng)和變形都通過(guò)一組方程來(lái)描述。這些方程包括材料模型、接觸條件、邊界條件和載荷條件。例如,材料模型可以是彈性、塑性或彈塑性,接觸條件可以是剛性接觸或軟接觸,邊界條件可以是固定或自由,載荷條件可以是沖擊載荷或預(yù)加載荷。

####示例:汽車碰撞模擬

```text

*KEYWORD

*PART

*COMPONENT_SHELL

1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1

*NODE

1,0.0,0.0,0.0

2,1.0,0.0,0.0

3,1.0,1.0,0.0

4,0.0,1.0,0.0

*ELEMENT_SHELL

1,1,2,3,4

*MATERIAL_ELASTIC

1,7800.0,210000.0,0.3

*SECTION_SHELL

1,1,1,0.1

*INITIAL_VELOCITY

1,1,0.0,0.0,100.0

*CONTACT_PAIR

1,1,1,1

*END在這個(gè)例子中,我們定義了一個(gè)簡(jiǎn)單的四節(jié)點(diǎn)殼單元,代表汽車的一部分結(jié)構(gòu)。材料被設(shè)定為彈性材料,密度為7800kg/m^3,楊氏模量為210000MPa,泊松比為0.3。初始速度被設(shè)定為100m/s,模擬汽車在碰撞前的運(yùn)動(dòng)狀態(tài)。接觸對(duì)被定義,以模擬汽車與障礙物之間的碰撞。4.3subdir5.2爆炸與沖擊案例4.3.1爆炸與沖擊原理爆炸與沖擊模擬是LS-DYNA的另一個(gè)重要應(yīng)用,用于研究爆炸波的傳播、沖擊載荷對(duì)結(jié)構(gòu)的影響等。這類模擬通常涉及高速、高能量的事件,需要精確的材料模型和復(fù)雜的載荷條件。LS-DYNA通過(guò)其強(qiáng)大的顯式求解器,能夠處理這些極端條件下的動(dòng)力學(xué)問(wèn)題。4.3.2爆炸與沖擊內(nèi)容在爆炸與沖擊模擬中,LS-DYNA可以使用多種材料模型,如Johnson-Cook模型、Gruneisen模型等,來(lái)描述材料在極端條件下的行為。此外,LS-DYNA還提供了多種載荷條件,如爆炸載荷、沖擊載荷等,來(lái)模擬爆炸與沖擊事件。4.3.2.1示例:爆炸模擬*KEYWORD

*PART

*COMPONENT_SOLID

1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1

*NODE

1,0.0,0.0,0.0

2,1.0,0.0,0.0

3,1.0,1.0,0.0

4,0.0,1.0,0.0

*ELEMENT_SOLID

1,1,2,3,4

*MATERIAL_JOHNSON_COOK

1,7800.0,210000.0,0.3,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,

#后處理與結(jié)果分析

##6.1結(jié)果文件讀取與可視化

在LS-DYNA的后處理階段,讀取和可視化結(jié)果文件是關(guān)鍵步驟。LS-DYNA生成的結(jié)果文件通常包括二進(jìn)制的`.d3plot`文件和文本的`.dat`文件,這些文件包含了模擬過(guò)程中的所有數(shù)據(jù),如位移、速度、應(yīng)力、應(yīng)變等。為了有效地分析這些數(shù)據(jù),通常使用專門的后處理軟件或編程語(yǔ)言如Python。

###讀取結(jié)果文件

使用Python讀取LS-DYNA的`.d3plot`文件,可以借助`pyD3plot`庫(kù)。下面是一個(gè)示例代碼,展示如何讀取一個(gè)`.d3plot`文件:

```python

importpyD3plot

#讀取d3plot文件

d3plot=pyD3plot.d3plot("example.d3plot")

#獲取時(shí)間步信息

time_steps=d3plot.time_steps

#獲取應(yīng)力數(shù)據(jù)

stress_data=d3plot.stress

#獲取應(yīng)變數(shù)據(jù)

strain_data=d3plot.strain

#打印時(shí)間步信息

print("時(shí)間步信息:",time_steps)4.3.3可視化結(jié)果可視化結(jié)果通常涉及將數(shù)據(jù)映射到模型的幾何形狀上,以便直觀地理解模擬過(guò)程中的變化。使用pyD3plot庫(kù),可以將應(yīng)力或應(yīng)變數(shù)據(jù)可視化:importmatplotlib.pyplotasplt

frommpl_toolkits.mplot3dimportAxes3D

#創(chuàng)建3D圖

fig=plt.figure()

ax=fig.add_subplot(111,projection='3d')

#可視化應(yīng)力數(shù)據(jù)

d3plot.plot_stress(stress_data,ax=ax)

#顯示圖形

plt.show()4.42應(yīng)力應(yīng)變曲線提取從LS-DYNA的結(jié)果中提取應(yīng)力應(yīng)變曲線,對(duì)于理解材料在不同載荷下的行為至關(guān)重要。這通常涉及到從特定的單元或節(jié)點(diǎn)中提取數(shù)據(jù)。4.4.1提取應(yīng)力應(yīng)變數(shù)據(jù)假設(shè)我們想要從一個(gè)特定的單元中提取應(yīng)力應(yīng)變數(shù)據(jù),可以使用以下Python代碼:#提取特定單元的應(yīng)力應(yīng)變數(shù)據(jù)

unit_id=1234#假設(shè)單元ID為1234

unit_stress=d3plot.stress[unit_id]

unit_strain=d3plot.strain[unit_id]

#打印應(yīng)力應(yīng)變數(shù)據(jù)

print("單元應(yīng)力:",unit_stress)

print("單元應(yīng)變:",unit_strain)4.4.2繪制應(yīng)力應(yīng)變曲線有了應(yīng)力和應(yīng)變數(shù)據(jù),我們可以使用matplotlib庫(kù)來(lái)繪制應(yīng)力應(yīng)變曲線:#繪制應(yīng)力應(yīng)變曲線

plt.figure()

plt.plot(unit_strain,unit_stress)

plt.title('應(yīng)力-應(yīng)變曲線')

plt.xlabel('應(yīng)變')

plt.ylabel('應(yīng)力')

plt.grid(True)

plt.show()4.53動(dòng)力學(xué)響應(yīng)譜分析動(dòng)力學(xué)響應(yīng)譜分析是評(píng)估結(jié)構(gòu)在動(dòng)態(tài)載荷下響應(yīng)的一種方法,特別是在地震工程中。LS-DYNA可以輸出加速度、速度和位移的時(shí)間歷史數(shù)據(jù),這些數(shù)據(jù)可以用于生成響應(yīng)譜。4.5.1讀取時(shí)間歷史數(shù)據(jù)首先,我們需要讀取包含時(shí)間歷史數(shù)據(jù)的.dat文件:importnumpyasnp

#讀取dat文件

data=np.loadtxt("example.dat")

#分離時(shí)間、加速度、速度和位移數(shù)據(jù)

time=data[:,0]

acceleration=data[:,1]

velocity=data[:,2]

displacement=data[:,3]

#打印數(shù)據(jù)

print("時(shí)間:",time)

print("加速度:",acceleration)

print("速度:",velocity)

print("位移:",displacement)4.5.2生成響應(yīng)譜使用讀取的時(shí)間歷史數(shù)據(jù),我們可以生成響應(yīng)譜。這通常涉及到對(duì)數(shù)據(jù)進(jìn)行傅里葉變換,然后計(jì)算頻譜加速度或頻譜位移。在Python中,可以使用scipy庫(kù)來(lái)完成這些計(jì)算:fromscipy.signalimportwelch,find_peaks

#計(jì)算頻譜加速度

frequencies,spectrum=welch(acceleration,fs=1/(time[1]-time[0]),nperseg=1024)

#找到峰值

peaks,_=find_peaks(spectrum,height=0)

#繪制響應(yīng)譜

plt.figure()

plt.plot(frequencies[peaks],spectrum[peaks])

plt.title('響應(yīng)譜')

plt.xlabel('頻率(Hz)')

plt.ylabel('頻譜加速度')

plt.grid(True)

plt.show()通過(guò)上述步驟,我們可以有效地從LS-DYNA的模擬結(jié)果中提取和分析關(guān)鍵數(shù)據(jù),從而更好地理解結(jié)構(gòu)的動(dòng)力學(xué)行為。5高級(jí)功能與技巧5.1自定義材料模型在LS-DYNA中,自定義材料模型允許用戶根據(jù)特定的物理特性或?qū)嶒?yàn)數(shù)據(jù)來(lái)定義材料的行為。這通常用于模擬標(biāo)準(zhǔn)材料模型無(wú)法準(zhǔn)確描述的復(fù)雜材料特性。自定義材料模型通過(guò)用戶定義的子程序(UMAT)實(shí)現(xiàn),這些子程序可以使用Fortran或C語(yǔ)言編寫。5.1.1原理自定義材料模型的核心是實(shí)現(xiàn)材料的應(yīng)力-應(yīng)變關(guān)系。在UMAT子程序中,用戶需要定義材料的本構(gòu)關(guān)系,包括彈性、塑性、蠕變、損傷等行為。此外,還需要考慮材料的熱效應(yīng)、加載速率依賴性等因素。5.1.2內(nèi)容UMAT子程序通常包括以下部分:初始化:設(shè)置材料參數(shù),如彈性模量、泊松比、屈服強(qiáng)度等。應(yīng)力計(jì)算:根據(jù)應(yīng)變和應(yīng)變率計(jì)算應(yīng)力。本構(gòu)關(guān)系更新:更新材料的內(nèi)部狀態(tài)變量,如塑性應(yīng)變、損傷變量等。熱效應(yīng)處理:如果材料行為受溫度影響,需要處理熱效應(yīng)。輸出:返回計(jì)算的應(yīng)力和材料狀態(tài)變量。5.1.3示例以下是一個(gè)簡(jiǎn)單的UMAT子程序示例,使用Fortran語(yǔ)言編寫,用于模擬線性彈性材料:SUBROUTINEUMAT(STRESS,DSTRESS,STRAIN,DSTRN,TIME,DTIME,TEMP,DTEMP,

&PREDEF,DPRED,NPREDF,PRESTN,DPREST,NPREST,NSTRN,

&NSTMN,NFIELD,IFIELD,JFIELD,KFIELD,LFIELD,MFIELD,

&NUSER,IORD,ISTEP,IINC,JACOB,DROT,ROT,DRATE,RATE,

&DLOAD,LOAD,DAREA,AREA,DPARAM,PARAM,DSTATEV,STATEV,

&PROPS,NPROPS,COORDS,NDIM,NSIDE,IP,J,K,L,M,N,

&USERMAT,USERID,USERSEED,USERSET,USERPARM)

IMPLICITNONE

INTEGERIP,J,K,L,M,N,NSIDE,NDIM,NPROPS,NSTRN,NSTMN,NFIELD,

&IFIELD,JFIELD,KFIELD,LFIELD,MFIELD,NUSER,IORD,ISTEP,IINC,

&USERID,USERSEED,USERSET,USERPARM

REAL*8STRESS(NDIM,NDIM),DSTRESS(NDIM,NDIM),STRAIN(NDIM,NDIM),

&DSTRN(NDIM,NDIM),TIME,DTIME,TEMP,DTEMP,PREDEF(NPREDF),

&DPRED(NPREDF),PRESTN(NPREST),DPREST(NPREST),JACOB(NDIM,NDIM),

&DROT(NDIM,NDIM),ROT(NDIM,NDIM),DRATE(NDIM,NDIM),RATE(NDIM,NDIM),

&DLOAD(NDIM,NDIM),LOAD(NDIM,NDIM),DAREA(NDIM,NDIM),AREA(NDIM,NDIM),

&DPARAM(NUSER),PARAM(NUSER),DSTATEV(NSTMN),STATEV(NSTMN),

&PROPS(NPROPS),COORDS(NDIM)

!定義材料參數(shù)

REAL*8E,NU,DENSITY

E=PROPS(1)!彈性模量

NU=PROPS(2)!泊松比

DENSITY=PROPS(3)!密度

!計(jì)算應(yīng)力

DOI=1,NDIM

DOJ=1,NDIM

IF(I.EQ.J)THEN

STRESS(I,J)=E*STRAIN(I,J)*(1.0-NU)/(1.0-2.0*NU)

ELSE

STRESS(I,J)=E*NU*STRAIN(I,J)/(1.0-2.0*NU)

ENDIF

ENDDO

ENDDO

!更新材料狀態(tài)變量

!在這個(gè)簡(jiǎn)單的例子中,我們沒(méi)有狀態(tài)變量需要更新

!返回計(jì)算結(jié)果

RETURN

END5.1.4描述此示例展示了如何在LS-DYNA中使用UMAT子程序來(lái)定義一個(gè)線性彈性材料模型。在初始化部分,從PROPS數(shù)組中讀取材料參數(shù)。然后,根據(jù)胡克定律計(jì)算應(yīng)力。由于這是一個(gè)簡(jiǎn)單的線性彈性模型,沒(méi)有需要更新的狀態(tài)變量,因此省略了本構(gòu)關(guān)系更新部分。5.2用戶定義的接觸算法LS-DYNA允許用戶自定義接觸算法,以更精確地模擬復(fù)雜的接觸行為。用戶定義的接觸算法(UCON)可以處理非標(biāo)準(zhǔn)接觸條件,如摩擦、粘附、熱接觸等。5.2.1原理UCON子程序在接觸事件發(fā)生時(shí)被調(diào)用,用戶需要定義接觸力和接觸條件。接觸力的計(jì)算通?;诮佑|面的幾何信息、接觸速度、接觸壓力等因素。5.2.2內(nèi)容UCON子程序包括:接觸力計(jì)算:根據(jù)接觸條件計(jì)算接觸力。接觸條件更新:更新接觸狀態(tài),如接觸面的相對(duì)位置、接觸速度等。輸出:返回計(jì)算的接觸力和更新后的接觸狀態(tài)。5.2.3示例以下是一個(gè)UCON子程序的示例,用于模擬帶有摩擦的接觸:```fortranSUBROUTINEUCON(F,DF,U,V,A,T,DT,T0,T1,T2,T3,T4,T5,T6,T7,&T8,T9,T10,T11,T12,T13,T14,T15,T16,T17,T18,&T19,T20,T21,T22,T23,T24,T25,T26,T27,T28,&T29,T30,T31,T32,T33,T34,T35,T36,T37,T38,&T39,T40,T41,T42,T43,T44,T45,T46,T47,T48,&T49,T50,T51,T52,T53,T54,T55,T56,T57,T58,&T59,T60,T61,T62,T63,T64,T65,T66,T67,T68,&T69,T70,T71,T72,T73,T74,T75,T76,T77,T78,&T79,T80,T81,T82,T83,T84,T85,T86,T87,T88,&T89,T90,T91,T92,T93,T94,T95,T96,T97,T98,&T99,T100,T101,T102,T103,T104,T105,T106,T107,&T108,T109,T110,T111,T112,T113,T114,T115,T116,&T117,T118,T119,T120,T121,T122,T123,T124,T125,&T126,T127,T128,T129,T130,T131,T132,T133,T134,&T135,T136,T137,T138,T139,T140,T141,T142,T143,&T144,T145,T146,T147,T148,T149,T150,T151,T152,&T153,T154,T155,T156,T157,T158,T159,T160,T161,&T162,T163,T164,T165,T166,T167,T168,T169,T170,&T171,T172,T173,T174,T175,T176,T177,T178,T179,&T180,T181,T182,T183,T184,T185,T186,T187,T188,&T189,T190,T191,T192,T193,T

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