composite wing

美 　英

• 網(wǎng)絡(luò)復(fù)合式機(jī)翼；混合聯(lián)隊(duì)；復(fù)合材料機(jī)翼

例句

The method is coupled with ANSYS to accomplish the optimal design of one composite wing, and the weight is reduced distinctly.

結(jié)合大型通用有限元程序ANSYS，完成某復(fù)合材料機(jī)翼結(jié)構(gòu)打樣階段優(yōu)化設(shè)計(jì)，減重效果明顯，并就計(jì)算中發(fā)現(xiàn)的問題對(duì)靈敏度分析進(jìn)行展望。

His suggestion led directly to the creation of the Chinese American Composite Wing.

他的意見直接導(dǎo)致了中美空軍混合編隊(duì)的成立。

Study of aeroelastic tailoring of high-aspect-ratio flexible composite wing

大展弦比柔性復(fù)合材料機(jī)翼的氣動(dòng)彈性剪裁

Research of the buckling stability analysis and optimum design of a composite wing based on the submodel technique

基于子模型的大型復(fù)合材料飛機(jī)結(jié)構(gòu)屈曲穩(wěn)定性數(shù)值分析及優(yōu)化技術(shù)研究

Composite Wing Structure Dynamics Design Subjected to Requirements of Natural Frequency and Position of Nodal Line

滿足固有頻率和振型要求的復(fù)合材料翼面結(jié)構(gòu)動(dòng)力學(xué)設(shè)計(jì)

Study of Nonlinear Flutter of High-aspect-ratio Composite Wing

大展弦比復(fù)合材料機(jī)翼的非線性顫振分析

Flutter analysis of an intelligent composite wing

智能復(fù)合材料機(jī)翼顫振分析

Dynamic Modeling and Flutter Analysis for High-Aspect-Ratio Composite Wing

復(fù)合材料大展弦比機(jī)翼動(dòng)力學(xué)建模與顫振分析

Stall Flutter Analysis of High-Aspect-Ratio Composite Wing

大展弦比復(fù)合材料機(jī)翼失速顫振分析