2018届九年级化学上册第4章认识化学变化第3节化学方程式第2课时导学案无答案沪教版201901162127.doc

上传人:postpastor181 文档编号:969320 上传时间:2019-03-11 格式:DOC 页数:2 大小:27.50KB
下载 相关 举报
2018届九年级化学上册第4章认识化学变化第3节化学方程式第2课时导学案无答案沪教版201901162127.doc_第1页
第1页 / 共2页
2018届九年级化学上册第4章认识化学变化第3节化学方程式第2课时导学案无答案沪教版201901162127.doc_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述

1、0第三节 化学方程式(第二课时)一、目标定向1、知道化学方程式表示的意义。2、能根据化学方程式进行计算。二、个体自学(阅读教材、思考问题)可能用的相对原子质量:H-1,O-16,Ca-40,C-12,Cl-35.5,Mg-241、写出右边化学方程式表示的意义:2H 2 + O2 点燃 2H 2O(1) (2) (3) 2、在 2CO + O2 点燃 2CO2反应中, 份质量的 CO 与 份质量的 O2反应生成 份质量的 CO2,三者的质量比是 : : 。3、观看书 107 页上方计算题的解答格式,模仿完成下列计算。碳酸钙与稀盐酸反应生成二氧化碳,若制备 4.4g 的二氧化碳,至少需要碳酸钙多少

2、 g?三、同伴互导1、小组内相互交流基础知识的对错。2、小组选出代表展示基础学习的成果。四、教师解难1、观看书 107 页的观察与思考,比较两种计算方法有什么不同,为什么都能得出正确的答案?2、利用反应前后物质的质量差进行的计算。为了测定某石灰石样品中碳酸钙的含量,取 10g 样品于烧杯中,再加入稀盐酸 50g,恰好完全反应(石灰石中的杂质不反应) ,反应后烧杯中物质的质量总和为 56.7g,求:石灰石样品中碳酸钙的质量?五、练习检测11、写出电解水的化学方程式 ,从该化学方程式中你能获得哪些信息?(1) (2) (3) 2、将 6g 的碳完全燃烧,参加反应的氧气质量是多少?六、补充学习1、工业上用电解氯化镁的方法生产金属镁:MgCl 2 通电 Mg + Cl 2电解 950kg 氯化镁至多能生产多少 kg 的镁,同时能得到多少 kg 氯气?

展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-RM-L55D08-1955 Exploratory investigation at Mach number 4 06 of an airplane configuration having a wing of trapezoidal plan form effects of various tail arrangements on water.pdf NASA NACA-RM-L55D08-1955 Exploratory investigation at Mach number 4 06 of an airplane configuration having a wing of trapezoidal plan form effects of various tail arrangements on water.pdf
  • NASA NACA-RM-L55G08-1955 Transonic wind-tunnel investigation of effects of windshield shape and canopy location on the aerodynamic characteristics of canopy-body combinations《挡风玻璃形.pdf NASA NACA-RM-L55G08-1955 Transonic wind-tunnel investigation of effects of windshield shape and canopy location on the aerodynamic characteristics of canopy-body combinations《挡风玻璃形.pdf
  • NASA NACA-RM-L55J06-1956 Low-Speed Static Stability Characteristics of a Complete Model with an M-Wing in Mid and High Positions and with Three Horizontal-Tail Heights《在中间和高位置处带有M形.pdf NASA NACA-RM-L55J06-1956 Low-Speed Static Stability Characteristics of a Complete Model with an M-Wing in Mid and High Positions and with Three Horizontal-Tail Heights《在中间和高位置处带有M形.pdf
  • NASA NACA-RM-L55J25-1956 Wind-tunnel investigation at high subsonic speeds of some effects of fuselage cross-section shape and wing height on the static longitudinal and lateral st5 de.pdf NASA NACA-RM-L55J25-1956 Wind-tunnel investigation at high subsonic speeds of some effects of fuselage cross-section shape and wing height on the static longitudinal and lateral st5 de.pdf
  • NASA NACA-RM-L55L19-1956 Transonic wind-tunnel measurements of static lateral and directional stability and vertical-tail loads for a model with a 45 degrees sweptback wing《带有45后掠翼.pdf NASA NACA-RM-L55L19-1956 Transonic wind-tunnel measurements of static lateral and directional stability and vertical-tail loads for a model with a 45 degrees sweptback wing《带有45后掠翼.pdf
  • NASA NACA-RM-L55L21-1956 A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach numbe.pdf NASA NACA-RM-L55L21-1956 A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach numbe.pdf
  • NASA NACA-RM-L56A10-1956 Low-speed longitudinal aerodynamic characteristics of a 45 degrees sweptback wing with double slotted flaps《带有双开缝襟翼的45后掠翼的低速纵向空气动力特性》.pdf NASA NACA-RM-L56A10-1956 Low-speed longitudinal aerodynamic characteristics of a 45 degrees sweptback wing with double slotted flaps《带有双开缝襟翼的45后掠翼的低速纵向空气动力特性》.pdf
  • NASA NACA-RM-L56C21-1956 Jet effects on base and afterbody pressures of a cylindrical afterbody at transonic speeds《在跨音速下 圆柱形飞机后体底部和后体压力的射流效应》.pdf NASA NACA-RM-L56C21-1956 Jet effects on base and afterbody pressures of a cylindrical afterbody at transonic speeds《在跨音速下 圆柱形飞机后体底部和后体压力的射流效应》.pdf
  • NASA NACA-RM-L56D03-1956 Low-speed wind-tunnel results for a thin aspect-ratio-1 85 pointed-wing-fuselage model with double slotted flaps《对带有双开缝襟翼且展弦比为1 85的突出机翼和机身模型的低速风洞研究结果》.pdf NASA NACA-RM-L56D03-1956 Low-speed wind-tunnel results for a thin aspect-ratio-1 85 pointed-wing-fuselage model with double slotted flaps《对带有双开缝襟翼且展弦比为1 85的突出机翼和机身模型的低速风洞研究结果》.pdf
  • 相关搜索

    当前位置:首页 > 考试资料 > 中学考试

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1