The aeroelastic phenomena may be subdivided under the heading static and dynamic . 氣動彈性現(xiàn)象可以再分為靜態(tài)和動態(tài)兩個專題。
Aeroelastic analysis of flexible large aspect ratio wing 特大展弦比機(jī)翼的特性與設(shè)計
Wind tunnel studies on the behaviour of aeroelastic twin cable model 串列雙索氣彈模型的風(fēng)洞試驗研究
Structural modeling and aeroelastic analysis of high - aspect - ratio composite wings 飛翼飛機(jī)穩(wěn)定性與操縱性研究
An effective transonic inverse design method for aeroelastic wing 基于控制理論方法的跨聲速彈性機(jī)翼反設(shè)計方法研究
The different influences of temperature to two aeroelastic systems are analyzed 分析了溫度對這兩種熱結(jié)構(gòu)氣動彈性系統(tǒng)的不同影響。
Mathematical model and formulations of a new tilt - rotor aircraft for aeroelastic stability analysis 新型傾轉(zhuǎn)旋翼機(jī)氣動彈性穩(wěn)定性分析模型
The multi - body analysis of the aeroelastic stability of the tiltrotor aircraft is presented 摘要通過多體動力學(xué)方法建立了傾轉(zhuǎn)旋翼機(jī)動力學(xué)分析模型。
Model experiment and damping identification for aeroelastic stability of helicopter rotor with elastomeric lag damper 帶粘彈減擺器旋翼系統(tǒng)氣彈穩(wěn)定性試驗與阻尼識別
Finally for all the above aeroelastic problems , distributed parallel computation is accomplished 最后對以上氣動彈性問題的數(shù)值計算進(jìn)行了基于微機(jī)網(wǎng)絡(luò)的分布式并行計算研究。