翼
- 基本解釋 (translations)
- ala · limb · pinna · pinnate · wing · pinnated · alette · pinnae · alae · limbing
- 詞組短語(yǔ)
- the wing of a bird
- 更多網(wǎng)絡(luò)例句與翼相關(guān)的網(wǎng)絡(luò)例句 [注:此內(nèi)容來(lái)源于網(wǎng)絡(luò)亚洲视频86p,僅供參考]
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The instructive conclusion was: 1 under the vertical loading, the shear-lag effect was produced badly, more severer under concentrated loading than under uniform loading .2 the longitudinal bending deformation of the beam flange was true of the imitating plane assumption of deformation . 3 the width length ratio was confirmed as the first factor working on the shear-lag effect among all the geometric parameters;4 the shear-lag coefficient of simple-supported box-girder was severer than the continuous box-girder, the shear-lag effect in the inner supported section of continuous beam was much more severer, we need paying more attention for it in designing. 5 the non-liner characteristics of material deformation have littlie influence on shear-lag effect in BGCW. 6 the experiential calculating formulation and calculating diagram for the effective flange width was raised with the only factor of the width-span ratio., but the primary location of axis of bending moments should not be changed while calculating the inertial moment .
研究認(rèn)為:1室內(nèi)模型試驗(yàn)和空間有限元分析結(jié)果均表明波形鋼腹板組合箱梁在豎向荷載作用下国产高清一级做a爱在线观看,翼板出現(xiàn)了典型的縱向應(yīng)力剪滯效應(yīng)在线毛片免费。2在豎向荷載作用下欧美性爱黄页,截面高度上各點(diǎn)縱向正應(yīng)變分布認(rèn)為可符合"擬平截面假定",以此作為波形鋼腹板組合箱梁抗彎計(jì)算的基本假定成人偷乱人伦精品视频在线观看网站。3箱梁寬跨比是影響波形鋼腹板組合箱梁翼板剪滯效應(yīng)的主要因素色喲喲国产精品。4連續(xù)波形鋼腹板組合箱梁的翼板剪滯系數(shù)大于簡(jiǎn)支梁谁有可以直接看av的网站,且連續(xù)箱梁內(nèi)支點(diǎn)截面翼板剪滯效應(yīng)相當(dāng)嚴(yán)重,對(duì)此需十分重視免费一极a毛片免费视频。5當(dāng)混凝土翼板受力由彈性階段進(jìn)入彈塑性階段時(shí),材料的非線性特性對(duì)翼板的剪滯效應(yīng)影響甚微怡红院老首页主页入口。6提出了根據(jù)組合箱梁的寬跨比參數(shù)來(lái)計(jì)算翼板有效寬度比的經(jīng)驗(yàn)公式和計(jì)算圖表免费在线日本视频,但箱梁截面抗彎慣性矩的計(jì)算不應(yīng)改變?cè)鹊慕孛嬷泻洼S位置。
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Ln this paper the effect of the position and planform of the canard wing on the burst process of the leading edge vortices over thedouble delta wing and the aerodynamic characteristics of the fighterconfiguration with the double delta wing are presented Furthermore,optimum fighter with the canard-double delta wing has been given.
本文給出了鴨翼對(duì)雙三角翼氣動(dòng)特性及渦的發(fā)展和破裂過(guò)程的影響亚洲欧美自拍另类日韩,進(jìn)而分析了鴨翼位置全免费又大粗又黄又爽、平面形狀對(duì)全機(jī)氣動(dòng)特性影響的機(jī)理,并提出了合理的鴨翼雙三角翼布局形式欧美性爱A√视频在线。
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Materials and Methods: The normal pterygopalatine fossa and its communication of 100 cases (200 sides) were studied, moreover pathological changes were observed in 23 cases (41 sides) of fibrous dysplasia by MSCT scanner, all volume data were subjected to multiplanar reformation, curved planar reformation in working station, to review the morphologic characteristics of the normal pterygopalatine fossa and its communications, to measure and compare the pterygopalatine fossa, pterygoid canal, foramen rotundum between two sets respectively.
資料與方法:對(duì)100例(200側(cè))正常翼腭窩及其通道及23例(41側(cè))累及翼腭窩及其通道骨纖維異常增殖癥患者進(jìn)行MSCT掃描后国产男女激情一区二区,將以上兩組所有數(shù)據(jù)傳至工作站進(jìn)行后處理重建,主要包括MPR在线视频懂、CPR91午夜黄色视频,觀察正常翼腭窩及其通道形態(tài)特征,并對(duì)兩組翼腭窩久久网色、翼管欧美性中文、圓孔的有關(guān)徑線進(jìn)行測(cè)量、比較国产无遮挡又黄又爽免费网站。
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In addition, the computational evaluations indicate that the heat transfer enhancement of delta winglet for aligned tube bank heat exchanger is more significant than that for staggered tube bank heat exchanger, the heat transfer enhancement of delta winglet with the attack angle of 45° is more obvious than that of 30°; the delta winglet with the attack angle of 45° leads to an increase in pressure drop, while the delta winglet with the attack angle of 30° results in a slight decrease.
另外計(jì)算還發(fā)現(xiàn):三角形小翼對(duì)順排換熱器的強(qiáng)化換熱效果好于對(duì)叉排換熱器的強(qiáng)化色播66;沖角為45°的三角形小翼強(qiáng)化換熱效果好于沖角為30°的三角形小翼;沖角為45°的三角形小翼導(dǎo)致空氣壓降提高国产精品一线在线播放,而沖角為30°的三角形小翼則可使壓降有所減小久久强奸网址。
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Qingyang pterosaur found before only found in the Junggar pterosaur fossils of the Cretaceous pterosaur is even; and Qingyang pterosaur pterosaur Junggar than earlier, more primitive Chiroptera late Jurassic pterosaur dragon type.
慶陽(yáng)翼龍發(fā)現(xiàn)之前,僅僅在新疆準(zhǔn)噶爾發(fā)現(xiàn)過(guò)翼龍化石国产专区自拍,尚且是白堊紀(jì)的翼龍国产美女一级牲交片在线观看;而慶陽(yáng)翼龍是比準(zhǔn)噶爾翼龍更早、更原始的晚侏羅紀(jì)翼手龍類(lèi)翼龍福利视频免费。
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Infratemporal space and parapharyngeal space were divided by the line from styloid process to medial or lateral pterygoid plate. Lateral pterygoid, styloid process, medial pterygoid plate and lateral pterygoid plate were important anatomical marks for imaging diagnosis.
自莖突至翼突內(nèi)側(cè)板后緣或翼突外側(cè)板前緣的連線可區(qū)分顳下間隙與咽旁間隙亚洲网络在线,翼外肌、莖突手噜国产、翼突內(nèi)側(cè)板和翼突外側(cè)板是CT等影像診斷的重要解剖學(xué)標(biāo)志99这里只有精品99。
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The land vehicle that is defined in claim 11, wherein said airfoil system includes at least three substantially vertical airfoils, said one airfoil being located essentially in a vertical plane containing the longitudinal axis of the vehicle, and the other two vertical airfoils being located at generally parallel relation to said one airfoil on opposite sides thereof rearwardly of the center of gravity of the vehicle.
土地車(chē)輛是指在索賠11 ,其中說(shuō)精品国产污污的网站,翼型系統(tǒng),一级不卡黄色视频免费观看,其中至少有三個(gè)大大的垂直翼型說(shuō),一翼型位于基本上是在一個(gè)垂直平面載有縱向軸的車(chē)輛男女赤裸裸插鸡视频在线观看,和其他兩個(gè)垂直翼型正位于普遍平行的關(guān)系說(shuō)91色国产在线,一翼型對(duì)對(duì)立面存在的rearwardly該中心的重心的車(chē)輛午夜AV福利网站。
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A wind- and motor-powered land vehicle with a fore-and-aft longitudinal axis comprising a body supported by wheels, at least one of said wheels fixed to rotate in a plane parallel to the fore-and-aft axis of said vehicle, an airfoil system comprised of two vertically extending airfoils rigidly mounted on said body in an arrangement having bilateral symmetry about a vertical plane through said fore-and-aft axis, said airfoil system providing a forward propelling force of said vehicle when the airfoil system is subjected to certain cross wind conditions, and self-contained motor propulsion means on said vehicle for providing acceleration from a stationary position and for propelling the vehicle either independently or in combination with propelling forces generated by wind action on said airfoil system, each airfoil having a plurality of airfoil sections telescopically fitted together, the lower airfoil section being rigidly mounted in fixed relationship to said body, said airfoil system including a retracting mechanism for lowering upper airfoil sections of said airfoil system when desired and for subsequently extending said airfoil system, said retracting mechanism including a plurality of linkages interconnecting said sections and an actuator means operatively connected between said body and to said linkages for lowering and extending each airfoil, and an intermediate airfoil extending between the upper sections of each of said airfoils so as to provide an inverted U-shaped airfoil.
風(fēng)力和電動(dòng)機(jī)驅(qū)動(dòng)的陸地車(chē)輛與前列和尾部長(zhǎng)軸組成的一個(gè)機(jī)構(gòu)的支持,車(chē)輪日韩在线精品色欲视频播放网站免费,至少有一說(shuō)A片视频在线一区二区,車(chē)輪固定在一個(gè)旋轉(zhuǎn)平面平行的前列和前后軸的說(shuō),車(chē)輛好男人社区影视在线,翼型系統(tǒng)組成的兩個(gè)垂直擴(kuò)展翼型硬性安裝在說(shuō)欧美日韩va视频,機(jī)構(gòu)在安排后,雙邊對(duì)稱(chēng)約一垂直面說(shuō)欧美自拍日韩经典,通過(guò)國(guó)內(nèi)外和前后軸女人天堂天天色,表示翼型系統(tǒng)提供了一個(gè)向前推進(jìn)的力量說(shuō),車(chē)輛時(shí)97碰碰碰免费人妻,翼型系統(tǒng)是受到某些橫風(fēng)條件下超碰夜晚人人爽人人爱,和自我載電機(jī)推進(jìn)的手段就表示,車(chē)輛提供加速?gòu)囊粋€(gè)固定的立場(chǎng)和為推進(jìn)車(chē)輛單獨(dú)或結(jié)合手机看片日韩av人人爽人人操,與推進(jìn)力量所產(chǎn)生的風(fēng)的行動(dòng)表示翼型系統(tǒng)十八岁以下免费观看黄色网站,每個(gè)機(jī)翼有一個(gè)多元化翼型第telescopically裝在一起,較低的翼型節(jié)被硬性安裝在固定的關(guān)系影音先锋图片资源站,說(shuō)身體国产爱在线,說(shuō)翼型系統(tǒng)包括一個(gè)撤消的機(jī)制,降低上翼型章節(jié)說(shuō)久久avabb,翼型系統(tǒng)時(shí)粉色视频又黄又爽免费,理想的和其后再將說(shuō),翼型制度毛片无码午夜国产视频,說(shuō)收回機(jī)制包括多元化的聯(lián)系互連說(shuō)免费的一级毛片,部分和一個(gè)致動(dòng)器的手段手術(shù)之間的連接說(shuō),身體和說(shuō)在线中文字幕日本,聯(lián)系降低717电影院理论片在线观看,并延長(zhǎng)每翼型,及一個(gè)中間翼型延長(zhǎng)之間的路段上的每說(shuō)翼型尤物在线观看视频,以便提供一個(gè)倒U -形翼型国产精品永久免费啪啪啪。
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One type of blade airfoil with high efficiency of a general axial flow fan is adopted as original airfoil, and it is shortened according to different length scale, and then joined to the exportation circular arc of the original airfoil in the opposite direction. Assuring the streamline on the surface of the blade profile after smooth operation, a new kind of double-head anti-unsymmetrical S model airfoils has been structured to be researched in this paper.
采用一種效率比較高的普通風(fēng)機(jī)葉片翼型作為原始翼型,按不同長(zhǎng)度比例縮小原始翼型影音先锋2020aⅴ色资源网,反向搭接在原始翼型的出口圓弧處国产精品自拍在线,經(jīng)過(guò)光滑處理,保證葉型表面的流線形后久久精品亚洲日本波多野结衣,構(gòu)成本文所研究的新型雙頭雙機(jī)翼反向S型不對(duì)稱(chēng)翼型91在线播放。
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Calibration tool storage cabinet rolling rack w/lights statu go rack rolling rack w/hardhats.tool.rarts metal work station office chairs 7"miter band saw fiberglass backing plates 12"band saw filing cabinets 7 air conditioners 6 humidifiers 2 grinders 2-carts w/testing equipment golf cart 6 utility carts left upper wing right upper wing 4 rolls of final bagging disassembled lay up room lexan 4*8*9/8 3 roof top air ducts preforming core fuselage to wing part non conforming steel/alominum insulation tubes left lower wing right lower wing horizontal upper tail 2 sheets of 1honeycomb core office cubicles cabin door frame template 1 medium size cabinet 2 small cabinets flammable container L.H.boom inboard flap hinge(2) R.H.boom inboard flap hinge(1) L.H.outboard nacelle little fuse CSL mold AFT keelgusset mold LH boom inboard mold RH boom outboard mold LH upper fuel tank mold RH lower fuel tank mold universal safety mats(13) aileron bond/drill jigs metal saw hooses 5-lay up tables safety mat trim kit empty rack office chairs left assembled boom right assembled boom utility carts small file cab bagging material black med.
標(biāo)定工具儲(chǔ)藏柜軋制機(jī)架瓦特/燈 statu去機(jī)架軋制機(jī)架瓦特/ hardhats.tool.rarts 金屬工作站辦公椅 7 &字帶鋸玻纖板支持 12 &帶鋸檔案柜 7空調(diào) 6加濕器 2磨床 2 ,車(chē)瓦/測(cè)試設(shè)備高爾夫球車(chē) 6實(shí)用車(chē)左上翼右上翼 4卷最后套袋拆卸積儲(chǔ)室聚碳酸酯4 * 8 * 9月8日 3天臺(tái)冷氣槽預(yù)成形核心機(jī)身的一部分中文字幕无码一级毛片免费,以翼不符合鋼鐵/ alominum 保溫管左下翼右下翼橫向上尾 2張1 蜂窩芯辦公室隔間艙門(mén)框模板 1中型內(nèi)閣 2小柜易燃集裝箱 L.H.boom內(nèi)側(cè)襟翼鉸鏈( 2 ) R.H.boom內(nèi)側(cè)襟翼鉸鏈( 1 ) L.H.outboard發(fā)動(dòng)機(jī)艙小保險(xiǎn)絲CSL的模具霉菌毒素keelgusset 黃體生成素臂船模生殖健康繁榮舷外模具激素上油箱模具相對(duì)濕度較低的燃料箱模具普遍安全墊( 13 )副翼債券/鉆夾具金屬看到hooses 5 -奠定表安全墊裝飾盒空架辦公椅離開(kāi)組裝繁榮正確組裝繁榮實(shí)用工具車(chē)小檔案駕駛室套袋材料黑色med东北老妓女叫床脏话对白视频。
- 更多網(wǎng)絡(luò)解釋與翼相關(guān)的網(wǎng)絡(luò)解釋 [注:此內(nèi)容來(lái)源于網(wǎng)絡(luò)亚洲欧美一区二区蜜臀图片,僅供參考]
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airfoil profile:翼型, 翼剖面
airfoil lift | 機(jī)翼升力, 翼型升力 | airfoil profile | 翼型, 翼剖面 | airfoil section | 翼剖面
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airfoil profile:翼切形,翼剖面
"airfoil lift coefficient","翼形升力系數(shù)" | "airfoil profile","翼切形,翼剖面" | "airfoil section","翼剖面,翼切面"
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Autogiro:旋翼機(jī)
自轉(zhuǎn)旋翼機(jī)(autogiro)是依靠無(wú)自身動(dòng)力驅(qū)動(dòng)、可自由旋轉(zhuǎn)的旋翼提供升力飛行的飛行器(如圖1). 飛行中,旋翼本身無(wú)發(fā)動(dòng)機(jī)驅(qū)動(dòng)而是靠空氣作用力驅(qū)動(dòng)其自轉(zhuǎn),進(jìn)而產(chǎn)生升力. 旋翼僅在起動(dòng)時(shí)有自身動(dòng)力驅(qū)動(dòng),之后靠空氣作用力驅(qū)動(dòng).
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Autogiro:自轉(zhuǎn)旋翼機(jī)
自轉(zhuǎn)旋翼機(jī)(autogiro)是依靠無(wú)自身動(dòng)力驅(qū)動(dòng)直接观看黄网站免费裸体赌场网站、可自由旋轉(zhuǎn)的旋翼提供升力飛行的飛行器(如圖1). 飛行中,旋翼本身無(wú)發(fā)動(dòng)機(jī)驅(qū)動(dòng)而是靠空氣作用力驅(qū)動(dòng)其自轉(zhuǎn),進(jìn)而產(chǎn)生升力. 旋翼僅在起動(dòng)時(shí)有自身動(dòng)力驅(qū)動(dòng),之后靠空氣作用力驅(qū)動(dòng).
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canard configuration:前翼構(gòu)型
"canard","前翼" | "canard configuration","前翼構(gòu)型" | "canard-delta configuration","前翼三角翼構(gòu)形"
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delta wing:三角翼
航空設(shè)計(jì)人員將其定義為主翼前緣后掠角超過(guò)45度,而后緣后掠角為0度,無(wú)水平安定面,謂之三角翼(Delta wing)翼形. 因主翼后掠角相當(dāng)大,故飛行速度在馬赫2以上時(shí),主翼前緣仍在馬赫錐內(nèi),氣流震波阻力低. 此類(lèi)主翼無(wú)水平安定面構(gòu)型之飛機(jī),
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pterygopalatine fossa:翼腭窩
翼腭窩 翼腭窩(pterygopalatine fossa)為居于上頜骨與翼突之間的狹窄骨性腔隙,其前界為上頜骨,后界為翼突及蝶骨大翼的前面,頂為蝶骨體之下面,內(nèi)側(cè)壁為腭骨的垂直部.
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hydrofoil boat:水翼艇=>水中翼船
hydrofoil amphibian 水翼式水陸兩用車(chē) | hydrofoil boat 水翼艇=>水中翼船 | hydrofoil control system 水翼操縱系統(tǒng)
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hydrofoil boat:水翼艇
hydrofoil 水翼,水翼船,水翼艇的雙翼 | hydrofoil amphibian 水翼式水陸兩用車(chē) | hydrofoil boat 水翼艇=
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leading edge:翼前緣
通常設(shè)計(jì)圖上都有標(biāo)示最高線所在,若圖上沒(méi)有標(biāo)示,則可自行將其標(biāo)在翼弦(Chord)長(zhǎng)度之30%~35%處.接著在最高線距翼前緣(Leading edge)的 1/2處畫(huà)上一條線,及最高線離翼后緣(Trailing edge)的 2/3處畫(huà)上一條線.并在翼前緣及后緣各畫(huà)上一條高度約1mm左右的水平線.