2018_2019版高中英语Unit1TalesoftheunexplainedVocabularybreakth讲义牛津译林必修2.doc

上传人:周芸 文档编号:1129041 上传时间:2019-05-08 格式:DOC 页数:4 大小:116.50KB
下载 相关 举报
2018_2019版高中英语Unit1TalesoftheunexplainedVocabularybreakth讲义牛津译林必修2.doc_第1页
第1页 / 共4页
2018_2019版高中英语Unit1TalesoftheunexplainedVocabularybreakth讲义牛津译林必修2.doc_第2页
第2页 / 共4页
2018_2019版高中英语Unit1TalesoftheunexplainedVocabularybreakth讲义牛津译林必修2.doc_第3页
第3页 / 共4页
2018_2019版高中英语Unit1TalesoftheunexplainedVocabularybreakth讲义牛津译林必修2.doc_第4页
第4页 / 共4页
亲,该文档总共4页,全部预览完了,如果喜欢就下载吧!
资源描述

1、1Vocabulary breakthroughA组 前缀appear vi.disappear vi.消失,失踪miss vt.dismiss vt.不予考虑;解雇;解散count vdiscount n折扣agree vdisagree vi.不同意B组 后缀puzzle vpuzzled adj.困惑的,茫然的create vt.creature n动物;(具有某种特征的)人construct vt.construction n施工;建筑物possible adj.possibility n可能性journal njournalist n记者amaze vt.amazing adj.令人

2、惊奇(惊叹)的evident adj.evidence n证据injure vt.injury n伤害laugh vi.laughter n笑声,笑enthusiasm nenthusiastic adj.热情的;热烈的;满腔热情的state vt.statement n陈述;声明2hair nhairy adj.多毛的,毛茸茸的exist vi.existence n存在C组 合成n n.spaceship n宇宙飞船schoolboy n(学校的)男生D组 转化n v.witness目击,见证flash闪光,闪耀base以为基础award授予,奖励attack攻击;进攻reserve预订;

3、保留;储备link联系,关联prep. adv.aboard在(轮船、飞机、火车等)上;上(轮船、飞机、火车等)n adj.blank空白的;无表情的A组 同义词story ntale n.animal ncreature n.reporter njournalist n.harm ninjury n.proper adj.appropriate adj.check vexamine v.B组 反义词hire vt.dismiss vt.C组 形近词abroad adv.在国外aboard adv.在(轮船、飞机、火车等)上;上(轮船、飞机、火车等)attract v吸引attack v攻击;

4、进攻1背诵经典 In the statement,the witness tried to convince people with all the evidence concerning the case.规范默写32背诵经典 Its amazing that such a slight incident due to carelessness should lead to a major attack of the villagers.规范默写43背诵经典 The journalist reported that following the tracks on the ground hel

5、ped the police to find the only man who survived the accident.规范默写4背诵经典 We can hear laughter from the next room where a party organized by Mr Wang is being held.规范默写5背诵经典 It occurred to me that I might look for a private detective to find out why the new company which was linked with several big ones disappeared after an existence of three months.规范默写6背诵经典 Please fill up the blanks in the questionnaire on the construction of the local base and whoever disagrees can reserve his view.规范默写

展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-TR-1206-1954 A revised gust-load formula and a re-evaluation of v-g data taken on civil transport airplanes from 1933 to 1950《从1933年至1950年从民用飞机中提取的v-g数据的改进阵风荷载公式和重新评估》.pdf NASA NACA-TR-1206-1954 A revised gust-load formula and a re-evaluation of v-g data taken on civil transport airplanes from 1933 to 1950《从1933年至1950年从民用飞机中提取的v-g数据的改进阵风荷载公式和重新评估》.pdf
  • NASA NACA-TR-1218-1955 Effect of ground interference on the aerodynamic and flow characteristics of a 42 degree sweptback wing at Reynolds numbers up to 6 8 x 10(6)《当雷诺数为6 8x10(6)时.pdf NASA NACA-TR-1218-1955 Effect of ground interference on the aerodynamic and flow characteristics of a 42 degree sweptback wing at Reynolds numbers up to 6 8 x 10(6)《当雷诺数为6 8x10(6)时.pdf
  • NASA NACA-TR-1224-1955 Effects of wing position and fuselage size on the low-speed static rolling stability characteristics of a delta-wing model《机翼位置和机身尺寸对三角形机翼模型低速静态旋转稳定特性的影响》.pdf NASA NACA-TR-1224-1955 Effects of wing position and fuselage size on the low-speed static rolling stability characteristics of a delta-wing model《机翼位置和机身尺寸对三角形机翼模型低速静态旋转稳定特性的影响》.pdf
  • NASA NACA-TR-1234-1955 On the Kernel function of the integral equation relating the lift and downwash distributions of oscillating finite wings in subsonic flow《在亚音速流下 与有限振荡机翼升力和气流.pdf NASA NACA-TR-1234-1955 On the Kernel function of the integral equation relating the lift and downwash distributions of oscillating finite wings in subsonic flow《在亚音速流下 与有限振荡机翼升力和气流.pdf
  • NASA NACA-TR-1263-1956 Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 .pdf NASA NACA-TR-1263-1956 Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 .pdf
  • NASA NACA-TR-1268-1956 Theoretical calculations of the pressure forces and moments at supersonic speeds due to various lateral motions acting on thin isolated vertical tails《由于薄且单独.pdf NASA NACA-TR-1268-1956 Theoretical calculations of the pressure forces and moments at supersonic speeds due to various lateral motions acting on thin isolated vertical tails《由于薄且单独.pdf
  • NASA NACA-TR-1274-1956 Second-order subsonic airfoil theory including edge effects《二阶超音速机翼理论(包括边缘效应)》.pdf NASA NACA-TR-1274-1956 Second-order subsonic airfoil theory including edge effects《二阶超音速机翼理论(包括边缘效应)》.pdf
  • NASA NACA-TR-1281-1956 Flight determination of drag of normal-shock nose inlets with various cowling profiles at Mach numbers from 0 9 to 1 5《当马赫数为0 9至1 5时 带有多个整流罩轮廓的正震波头部进气道阻力的飞行测.pdf NASA NACA-TR-1281-1956 Flight determination of drag of normal-shock nose inlets with various cowling profiles at Mach numbers from 0 9 to 1 5《当马赫数为0 9至1 5时 带有多个整流罩轮廓的正震波头部进气道阻力的飞行测.pdf
  • NASA NACA-TR-1284-1956 Theory of wing-body drag at supersonic speeds《在超音速下机翼机身阻力的理论》.pdf NASA NACA-TR-1284-1956 Theory of wing-body drag at supersonic speeds《在超音速下机翼机身阻力的理论》.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