aeroelastic tailoring中文是什么意思

發(fā)音:

中文翻譯
造句

氣動彈性裁剪

tailoring n. 1.裁縫業(yè)，成衣業(yè)。 2.裁縫法，縫工。
aeroelastic 變形的; 氣動力彈性的
aerodynamic tailoring 氣動裁剪
curriculum tailoring 課程剪裁
handcraft tailoring 工藝裁縫
program tailoring 程序裁剪
tailoring machine 成衣機(jī)
tailoring process 剪裁過程
tailoring trainer 城市里找到裁縫導(dǎo)師
terminal tailoring 終端機(jī)裁整
aeroelastic characteristics 氣動彈性特性
aeroelastic constraints 空氣動力彈性限制
aeroelastic derivative 氣動彈性導(dǎo)數(shù)
aeroelastic distortion 氣動力彈性變形
aeroelastic distribution 氣動力彈性分布
aeroelastic divergence 氣動彈性發(fā)散
aeroelastic effect 空氣彈性效應(yīng); 氣動彈性效應(yīng)
aeroelastic effects 氣動彈性效應(yīng)
aeroelastic influence 空氣彈性效應(yīng)
aeroelastic instability 氣動彈性不穩(wěn)定性
aeroelastic load 氣動彈性載荷
aeroelastic oscillations 氣動彈性振動
aeroelastic problem 空氣彈性問題
aeroelastic test 氣動彈性試驗
aeroelastic stability 氣動彈性穩(wěn)定性

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例句與用法

Combined with modem structural finite element analysis , modern structural optimization algorithms , composite structures mechanics and aeroelastic tailoring of composite wing as well as relative high performance numerical method , a system named the composite synthesis optimization for aircraft structures ( cosoas ) , has been developed in this paper , which has own independent component of finite element analysis
本文結(jié)合現(xiàn)代結(jié)構(gòu)有限元分析方法、現(xiàn)代結(jié)構(gòu)優(yōu)化算法、復(fù)合材料結(jié)構(gòu)力學(xué)、復(fù)合材料氣動彈性剪裁設(shè)計方法以及相關(guān)的高性能數(shù)值計算工具開發(fā)出了擁有自己獨立有限元程序的復(fù)合材料飛機(jī)結(jié)構(gòu)綜合優(yōu)化設(shè)計系統(tǒng)( cosoas ) 。在內(nèi)容上本文突出復(fù)合材料應(yīng)用特色。
Moreover , in the application of aircraft structures design , the composite wing is still to meet the needs of aeroelastic design . through reading the aerodynamic influence coefficient matrix from the nastran file , this paper generates a static aeroelastic equilibrium equation and divergence eigen - equation , which is needed by the aeroelastic tailoring of composite wing . through this equation , the aeroelastic tailoring of composite wing and its optimization design have come into being
此外在飛機(jī)結(jié)構(gòu)設(shè)計過程中，復(fù)合材料翼面結(jié)構(gòu)還要滿足氣動彈性設(shè)計的需要，本文通過讀入由nastran所產(chǎn)生的氣動影響系數(shù)矩陣，構(gòu)造出滿足復(fù)合材料氣動彈性分析所需要的靜氣動彈性平衡方程和發(fā)散特征方程，并在此基礎(chǔ)上實現(xiàn)了復(fù)合材料氣動彈性剪裁優(yōu)化設(shè)計。

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