(江苏专用)2020版高考英语新增分大一轮复习单词表词汇闪记Unit2Whatishappinesstoyou讲义牛津译林版选修6.doc

上传人:fuellot230 文档编号:1119297 上传时间:2019-05-01 格式:DOC 页数:2 大小:28.50KB
下载 相关 举报
(江苏专用)2020版高考英语新增分大一轮复习单词表词汇闪记Unit2Whatishappinesstoyou讲义牛津译林版选修6.doc_第1页
第1页 / 共2页
(江苏专用)2020版高考英语新增分大一轮复习单词表词汇闪记Unit2Whatishappinesstoyou讲义牛津译林版选修6.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、1Unit 2 What is happiness to yousurround vt.围绕,环绕suffering n.疼痛,痛苦;折磨viewer n.电视观众;观看者goodwill n.友好;善意junior adj.青少年的;地位(或职位、级别)低下的apart adv.分开,分离apart from 远离,和不在一起;除了mat n.(体育运动用的)厚垫子specialist n.专科医师;专家severe adj.严重的;严厉的,严格的;艰巨的in good spirits 心情好appreciation n.感激,感谢;欣赏;理解;(艺术方面的)鉴定,评估sorrow n.悲伤

2、悲痛accomplish vt.完成,实现thankful adj.感激的,感谢的adapt vi.& vt.(使)适应;改编broadcasting n.(无线电和电视的)节目制作和播放;广播advocate vt.拥护;支持;提倡admirable adj.令人钦佩的,令人羡慕的,值得赞美的rebuild vt.重建;改建unbearable adj.无法忍受的go after 追求;谋求alcohol n.含酒精的饮料;酒temporary adj.短暂的;暂时的depth n.最深处;深度;深厚soul n.灵魂ski vi.滑雪n.滑雪板accompany vt.陪伴,陪同;伴随;

3、为伴奏instructor n.教练;导师on ones own 独自,单独;独立地procedure n.步骤,程序directly adv.径直地;直接地2head for 朝方向(地方)行时,前往obey vt.& vi.服从,听从,顺从outstanding adj.优秀的,杰出的,出色的talent n.天资,天赋;天才allocate vt.分配adequate adj.足够的;合乎需要的quit vt.& vi.停止;放弃;离开uncertain adj.无把握的,不确定的golden adj.美好的;金色的;金的at that point 在那时;在那个阶段rush n.匆忙i

4、n a rush 匆忙地,急切地entertainment n.娱乐活动;娱乐;招待,款待hardship n.艰难,困苦ache vi.& n.疼痛vivid adj.清晰的,生动的,鲜明的predict vt.预言,预告,预报workday n.工作日part-time adj.& adv.部分时间的(地);兼职的(地)handy adj.易使用的;便利的assist vt.帮助,协助automatic adj.自动的instant adj.即食的,方便的;立刻的maximum adj.最多的,最大的 n 最大值,最大极限minimum adj.最少的,最小的 n.最小值,最小极限mature adj.成熟的vi.成熟;使充分发展motivation n.动力,动机

展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-RM-E54F11-1954 Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates《通过大量平行平板气流的实验性热传递和摩擦系数》.pdf NASA NACA-RM-E54F11-1954 Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates《通过大量平行平板气流的实验性热传递和摩擦系数》.pdf
  • NASA NACA-RM-E54I13-1954 Experimental investigation of drag of afterbodies with exiting jet at high subsonic Mach numbers《在亚音速马赫数下现有喷气式飞机的飞机后体阻力实验研究》.pdf NASA NACA-RM-E54I13-1954 Experimental investigation of drag of afterbodies with exiting jet at high subsonic Mach numbers《在亚音速马赫数下现有喷气式飞机的飞机后体阻力实验研究》.pdf
  • NASA NACA-RM-E57E06-1957 Jet effects on base pressures of conical afterbodies at Mach 1 91 and 3 12《在马赫数为1 91至3 12时 圆锥飞机后体基准压力的喷射影响》.pdf NASA NACA-RM-E57E06-1957 Jet effects on base pressures of conical afterbodies at Mach 1 91 and 3 12《在马赫数为1 91至3 12时 圆锥飞机后体基准压力的喷射影响》.pdf
  • NASA NACA-RM-H56C20-1956 Time-vector determined lateral derivatives of a swept-wing fighter-type airplane with three different vertical tails at Mach numbers between 0 70 and 1 48《.pdf NASA NACA-RM-H56C20-1956 Time-vector determined lateral derivatives of a swept-wing fighter-type airplane with three different vertical tails at Mach numbers between 0 70 and 1 48《.pdf
  • NASA NACA-RM-H56H03-1957 Dynamic longitudinal stability characteristics of a swept-wing fighter-type airplane at Mach numbers between 0 36 and 1 45《在马赫数为0 36至0 45时 掠翼战斗型飞机的动态纵向稳定性特.pdf NASA NACA-RM-H56H03-1957 Dynamic longitudinal stability characteristics of a swept-wing fighter-type airplane at Mach numbers between 0 36 and 1 45《在马赫数为0 36至0 45时 掠翼战斗型飞机的动态纵向稳定性特.pdf
  • NASA NACA-RM-L50A04-1950 Longitudinal characteristics of two 47 7 degrees sweptback wings with aspect ratios of 5 1 and 6 0 at Reynolds numbers up to 10 x 10(exp 6)《在雷诺数为10x10(指数6).pdf NASA NACA-RM-L50A04-1950 Longitudinal characteristics of two 47 7 degrees sweptback wings with aspect ratios of 5 1 and 6 0 at Reynolds numbers up to 10 x 10(exp 6)《在雷诺数为10x10(指数6).pdf
  • NASA NACA-RM-L50E26-1950 Damping in roll of rectangular wings of several aspect ratios and NACA 65A-series airfoil sections of several thickness ratios at transonic and supersonic ls《在.pdf NASA NACA-RM-L50E26-1950 Damping in roll of rectangular wings of several aspect ratios and NACA 65A-series airfoil sections of several thickness ratios at transonic and supersonic ls《在.pdf
  • NASA NACA-RM-L50F16-1950 Low-speed aerodynamic characteristics of a series of swept wings having NACA 65A006 airfoil sections《带有NACA65A006翼剖面的一系列掠翼的低速空气动力特性》.pdf NASA NACA-RM-L50F16-1950 Low-speed aerodynamic characteristics of a series of swept wings having NACA 65A006 airfoil sections《带有NACA65A006翼剖面的一系列掠翼的低速空气动力特性》.pdf
  • NASA NACA-RM-L50H29-1950 Positioning investigation of single slotted flaps on a 47 7 degrees sweptback wing at Reynolds numbers of 4 0 x 10(exp 6) and 6 0 x 10(exp 6)《在雷诺数为4 0x10(指.pdf NASA NACA-RM-L50H29-1950 Positioning investigation of single slotted flaps on a 47 7 degrees sweptback wing at Reynolds numbers of 4 0 x 10(exp 6) and 6 0 x 10(exp 6)《在雷诺数为4 0x10(指.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