二年级英语下册Module5Unit2Whatarethekidsplaying课件外研版(一起).ppt

上传人:diecharacter305 文档编号:1208999 上传时间:2019-05-27 格式:PPT 页数:15 大小:2.79MB
下载 相关 举报
二年级英语下册Module5Unit2Whatarethekidsplaying课件外研版(一起).ppt_第1页
第1页 / 共15页
二年级英语下册Module5Unit2Whatarethekidsplaying课件外研版(一起).ppt_第2页
第2页 / 共15页
二年级英语下册Module5Unit2Whatarethekidsplaying课件外研版(一起).ppt_第3页
第3页 / 共15页
二年级英语下册Module5Unit2Whatarethekidsplaying课件外研版(一起).ppt_第4页
第4页 / 共15页
二年级英语下册Module5Unit2Whatarethekidsplaying课件外研版(一起).ppt_第5页
第5页 / 共15页
点击查看更多>>
资源描述

Module 5 Unit 2,What are the kids playing?,Kids 孩子,Playground操场,Skip 跳绳,Football match 足球比赛,What are you doing?,Im catching them.,What are you doing?,Im catching them.,What are the kids playing?,They are running.,What are they playing?,Some are skipping.,Some are playing football match.,Homework,情景对话,运用本课句型角色表演掌握本课新单词,Thank you!,

展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-TN-1110-1946 Two-dimensional wind-tunnel investigation of an approximately 14-percent-thick NACA 66-series-type airfoil section with a double slotted flap《带有双开缝襟翼且大约厚度为14.pdf NASA NACA-TN-1110-1946 Two-dimensional wind-tunnel investigation of an approximately 14-percent-thick NACA 66-series-type airfoil section with a double slotted flap《带有双开缝襟翼且大约厚度为14.pdf
  • NASA NACA-TN-1113-1947 Collection and analysis of hinge-moment data on control-surface tabs《操纵面伺服片铰链力矩数据的采集和分析》.pdf NASA NACA-TN-1113-1947 Collection and analysis of hinge-moment data on control-surface tabs《操纵面伺服片铰链力矩数据的采集和分析》.pdf
  • NASA NACA-TN-1174-1947 The application of high-temperature strain gages to the measurements of vibratory stresses in gas-turbine buckets《高温应变计对气体涡轮机叶片中振动性应力测量的应用》.pdf NASA NACA-TN-1174-1947 The application of high-temperature strain gages to the measurements of vibratory stresses in gas-turbine buckets《高温应变计对气体涡轮机叶片中振动性应力测量的应用》.pdf
  • NASA NACA-TN-1175-1947 Lifting-surface-theory aspect-ratio corrections to the lift and hinge-moment parameters for full-span elevators on horizontal tail surfaces《在水平尾翼面上全翼展电梯升力和铰链.pdf NASA NACA-TN-1175-1947 Lifting-surface-theory aspect-ratio corrections to the lift and hinge-moment parameters for full-span elevators on horizontal tail surfaces《在水平尾翼面上全翼展电梯升力和铰链.pdf
  • NASA NACA-TN-1187-1947 Formulas for additional mass corrections to the moments of inertia of airplanes《附加质量更正和飞机惯性力矩的公式》.pdf NASA NACA-TN-1187-1947 Formulas for additional mass corrections to the moments of inertia of airplanes《附加质量更正和飞机惯性力矩的公式》.pdf
  • NASA NACA-TN-1191-1947 Two-dimensional wind-tunnel investigation of four types of high-lift flap on an NACA 65-210 airfoil section《NACA 65-210翼剖面上四种类型高升力襟翼的二维风洞研究》.pdf NASA NACA-TN-1191-1947 Two-dimensional wind-tunnel investigation of four types of high-lift flap on an NACA 65-210 airfoil section《NACA 65-210翼剖面上四种类型高升力襟翼的二维风洞研究》.pdf
  • NASA NACA-TN-1193-1947 Effect of product of inertia on lateral stability《惯性积对横向稳定性的影响》.pdf NASA NACA-TN-1193-1947 Effect of product of inertia on lateral stability《惯性积对横向稳定性的影响》.pdf
  • NASA NACA-TN-1197-1947 Some investigations of the general instability of stiffened metal cylinders VIII - stiffened metal cylinders subjected to pure torsion《硬化金属汽缸VIII一般稳定性的一些研究 承.pdf NASA NACA-TN-1197-1947 Some investigations of the general instability of stiffened metal cylinders VIII - stiffened metal cylinders subjected to pure torsion《硬化金属汽缸VIII一般稳定性的一些研究 承.pdf
  • NASA NACA-TN-1212-1947 Effect of reflex camber on the aerodynamic characteristics of a highly tapered moderately swept-back wing at Reynolds numbers up to 8 000 000《当雷诺数为8 000 000时.pdf NASA NACA-TN-1212-1947 Effect of reflex camber on the aerodynamic characteristics of a highly tapered moderately swept-back wing at Reynolds numbers up to 8 000 000《当雷诺数为8 000 000时.pdf
  • 相关搜索

    当前位置:首页 > 教学课件 > 中学教育

    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