2018_2019学年度八年级语文下册第五单元江山多娇基础检测新人教版.docx

上传人:孙刚 文档编号:952501 上传时间:2019-03-08 格式:DOCX 页数:4 大小:106.45KB
下载 相关 举报
2018_2019学年度八年级语文下册第五单元江山多娇基础检测新人教版.docx_第1页
第1页 / 共4页
2018_2019学年度八年级语文下册第五单元江山多娇基础检测新人教版.docx_第2页
第2页 / 共4页
2018_2019学年度八年级语文下册第五单元江山多娇基础检测新人教版.docx_第3页
第3页 / 共4页
2018_2019学年度八年级语文下册第五单元江山多娇基础检测新人教版.docx_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、1第五单元 基础检测一、汉字书写1.根据拼音在田字格里写出正确的汉字。2.下列词语中都有错别字,请将正确的汉字写在田字格里。二、古诗文默写3.孟浩然的望洞庭湖赠张丞相中,表达诗人渴望出仕而无人引荐的句子是:4.望洞庭湖赠张丞相一诗中,写出洞庭湖烟波浩渺、水天合一的宏伟气象的名句是:5.王勃的送杜少府之任蜀州中表明真挚的友情可以克服空间阻隔的诗句是:26.王勃的送杜少府之任蜀州中表明不要因为离别而伤感的诗句是:7.苏轼的卜算子黄州定慧院寓居作中,表现词人高洁自许,不愿随波逐流的心境的句子是:8.陆游的卜算子咏梅中,写梅花纵使凋落于地,仍是香气不改,精神犹在的句子是:三、病句修改9.下列句子中没有

2、语病的一项是 ( )A.傅雷以深厚的学养、真挚的父爱,倾听着万里之外儿子的每一次心跳和儿子前进路上可能出现的困难,用一封封的书信传递着自己的惦念。B.央视经典咏流传最大的创新点是将传统诗词经典与现代流行相结合,有了这种传承方式,中华优秀传统文化一定能在青少年中开花、生根、结果。C.“伸手的人生没滋味,拼搏的人生才幸福。 ”黄冈各级政府积极支持贫困户靠自己的努力走上脱贫致富,涌现了一批不等不靠的自主脱贫典型。D.文明是一种修养,这种修养是从日常生活的细节中一点一滴积累起来的,有时生活习惯中的细节才是一个人是否文明的最真实表现。四、文学常识与名著阅读10.判断下列说法是否正确。(错的打“” ,对的

3、打“”)(1)1920年,保尔在一次作战中头部、腹部多次受伤,右眼失去 80%的视力;1927 年3全身瘫痪,双目失明,完全失去了活动能力。他便开始了英雄主义事业文学创作,1934年出版了钢铁是怎样炼成的 。( )(2)钢铁是怎样炼成的分为两部分,第一部分描写国内战争,第二部分描写经济恢复和社会主义建设。( )(3)保尔的英勇表现在他驰骋疆场,骁勇善战,屡立战功上。( )4详解详析1诫 霎 推搡 驰骋 漩涡 噤 棱 骤 虔诚 恭顺 蠕 凄凉 懈怠 瞬息 喧哗 矗 映照 苍劲 翡翠 擦拭 前呼后拥 轻歌曼舞 纷至沓来2抚妩 燥躁 振震 扼遏 滕腾 跳眺 穿川 曼漫3欲济无舟楫 端居耻圣明4八月湖水平 涵虚混太清5海内存知己 天涯若比邻6无为在歧路 儿女共沾巾7拣尽寒枝不肯栖 寂寞沙洲冷8零落成泥碾作尘 只有香如故9解析 D 本题考查对语病的辨析。A 项,搭配不当, “倾听”和“困难”不能搭配;B 项,语序不当,正确语序应为“生根、开花、结果” ;C 项,成分残缺,应在“走上脱贫致富”后加上“的道路” 。10(1) (2) (3)

展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-RM-L52A29-1952 Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds aspect-ratio series《在高亚音速展弦比系列下.pdf NASA NACA-RM-L52A29-1952 Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds aspect-ratio series《在高亚音速展弦比系列下.pdf
  • NASA NACA-RM-L52B13-1952 Effects of some primary variables of rectangular vortex generators on the static-pressure rise through a short diffuser《矩形旋涡发生器的一些初级变量对通过短扩散器静态压力上升的影响》.pdf NASA NACA-RM-L52B13-1952 Effects of some primary variables of rectangular vortex generators on the static-pressure rise through a short diffuser《矩形旋涡发生器的一些初级变量对通过短扩散器静态压力上升的影响》.pdf
  • NASA NACA-RM-L52C11-1952 Low-speed longitudinal aerodynamic characteristics of a twisted and cambered wing of 45 degrees sweepback and aspect ratio 8 with and without high-lift andolds.pdf NASA NACA-RM-L52C11-1952 Low-speed longitudinal aerodynamic characteristics of a twisted and cambered wing of 45 degrees sweepback and aspect ratio 8 with and without high-lift andolds.pdf
  • NASA NACA-RM-L52E02-1952 Longitudinal frequency-response and stability characteristics of the Douglas D-558-II airplane as determined from transient response to a Mach number of 0 .pdf NASA NACA-RM-L52E02-1952 Longitudinal frequency-response and stability characteristics of the Douglas D-558-II airplane as determined from transient response to a Mach number of 0 .pdf
  • NASA NACA-RM-L52E06-1952 Effects of stabilizing fins and a rear-support sting on the base pressure of a body of revolution in free flight at Mach numbers from 0 7 to 1 3《当马赫数为0 7至1.pdf NASA NACA-RM-L52E06-1952 Effects of stabilizing fins and a rear-support sting on the base pressure of a body of revolution in free flight at Mach numbers from 0 7 to 1 3《当马赫数为0 7至1.pdf
  • NASA NACA-RM-L52G07-1952 Wind-tunnel investigation of the low-speed static and rotary stability derivatives of a 0 13-scale model of the Douglas D-558-II airplane in the landing co.pdf NASA NACA-RM-L52G07-1952 Wind-tunnel investigation of the low-speed static and rotary stability derivatives of a 0 13-scale model of the Douglas D-558-II airplane in the landing co.pdf
  • NASA NACA-RM-L52G18-1952 Investigation of the effects of variations in the Reynolds number between 0 4 x 10(exp 6) and 3 0 x 10(exp 6) on the low-speed aerodynamic characteristics ith .pdf NASA NACA-RM-L52G18-1952 Investigation of the effects of variations in the Reynolds number between 0 4 x 10(exp 6) and 3 0 x 10(exp 6) on the low-speed aerodynamic characteristics ith .pdf
  • NASA NACA-RM-L52J17-1956 An investigation at Mach numbers of 1 41 and 2 01 of the aerodynamic characteristics of a swept-wing supersonic bomber configuration《当马赫数为1 41至2 01时 掠翼超音速投.pdf NASA NACA-RM-L52J17-1956 An investigation at Mach numbers of 1 41 and 2 01 of the aerodynamic characteristics of a swept-wing supersonic bomber configuration《当马赫数为1 41至2 01时 掠翼超音速投.pdf
  • NASA NACA-RM-L52K06-1952 Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2 05 2 54 and 3 04《当马赫数为2 05 2 54和3 04时 半球形机头的压力分布和压力阻力》.pdf NASA NACA-RM-L52K06-1952 Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2 05 2 54 and 3 04《当马赫数为2 05 2 54和3 04时 半球形机头的压力分布和压力阻力》.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