1、

Mathematical model and formulations of a new tilt-rotor aircraft for aeroelastic stability analysis

新型倾转旋翼机气动弹性稳定性分析模型

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2、

Modeling study on tilt-rotor's aeroelastic stability in cruise flight Surface Improvement Based on Springback Compensation for Aircraft Skin Stretching Tool

前飞状态倾转旋翼机气弹稳定性建模基于回弹的飞机蒙皮拉形模型面修模技术研究

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3、

EVALUATION ON STATIC STABILITY OF OIL-IN-WATER VISCOUS CRUDE EMULSION Modeling study on tilt-rotor's aeroelastic stability in cruise flight

O/W型稠油乳状液的静态稳定性评价前飞状态倾转旋翼机气弹稳定性建模

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4、

Flying bomb ( missiles resembling aircraft) Modeling study on tilt-rotor's aeroelastic stability in cruise flight

飞弹(飞机的导弹)前飞状态倾转旋翼机气弹稳定性建模

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5、

Calculation and Stability Analysis on Integral Steel Side Formwork of Continuous Box-Girder in Qingdao Bay-Bridge Modeling study on tilt-rotor's aeroelastic stability in cruise flight

青岛海湾大桥箱梁整体钢侧模支架体系计算及抗倾覆稳定分析前飞状态倾转旋翼机气弹稳定性建模

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6、

An analytical model of tilt-rotor/ pylon/ wing coupled aeroelastic stability is presented and the dynamic equations are derived for a new semi-articulated, soft-inplane tilt-rotor aircraft.

针对新型半铰接式、摆振柔软的倾转旋翼机,建立了旋翼/动力舱/机翼气动弹性稳定性分析模型,并导出了系统的动力学方程。

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7、

Get the amplitude frequency characteristics of impulse response and aeroelastic coupling response by discrete Fourier transform of time domain response, then get the structural damping of blade and tower and the aeroelastic damping of blade based on half-power bandwidth method.

通过对时域响应进行离散傅里叶变换,得出脉冲响应与气弹耦合响应的幅频特性,然后基于半功率带宽法得出叶片与塔架的结构阻尼及叶片的气弹阻尼。

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8、

Rotor Aeroelastic Stability Modeling Based on Inertial Coordinate Frame

惯性坐标系下的旋翼气弹稳定性建模

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9、

Based on the Piston Theory of supersonic aerodynamics and the theory of thin shell with geometric nonlinearity, the aeroelasticity flutter equations of the thin shell in axial supersonic airflow are established in order to analyze the nonlinear flutter responses of the aeroelastic system.

为研究高速飞行薄壳的气动弹性非线性颤振响应,本文基于超音速气动力活塞理论和大变形几何非线性理论,建立了薄壳大挠度气动弹性颤振方程。

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10、

Aeroelastic response analysis of coupled rotor/ nacelle/ tower for a horizontal axis wind turbine

风力发电机耦合转子/机舱/塔架的气弹响应

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11、

Combining with the aerodynamic load model of blade, get the aeroelastic coupling response of blade under the action of constant wind speed and turbulence wind speed.

结合叶片气动载荷模型,得到了叶片在定风速及紊流风速作用下的气弹耦合响应。

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12、

An aeroelastic model design of ultra-high voltage power transmission line systems

特高压输电塔线体系的气动弹性模型设计

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13、

then the aeroelastic state-space model is built by rational function approximation.

利用气动力有理函数拟合,得到气动弹性状态空间模型。

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14、

In this paper a new idea to investigate flutter problem Is proposed, the new idea is that we may study only a tew modes of an aeroelastic system instead of studying the whole.

本文研究了弹性飞机的颤振主动抑制就颤振发生的实质的讨论,提出一种研究颤振问题的探索性想法,即把对全系统颤振问题的研究归结到对其中少数有关的运动模态特性的研究。

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15、

An applicaton of computer to netting unit webbing technology aeroelastic tailoring applied to composite wing

计算机在网片剪裁单元工艺中的应用复合材料翼面的气动弹性剪裁

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16、

Based on the potential flow theory and the thin plate bending theory, the governing motion equations of the aeroelastic panel models were obtained.

基于不可压缩流体势流理论亚音速气动力和弹性薄板弯曲理论建立薄板气动弹性耦合运动方程。

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17、

In the past wind tunnel investigations were the main way to study the aeroelastic problem. When evaluating the aeroelastic stability of a long-span bridge under wind, it is mostly assumed that wind normal to the bridge span is most unfavorable.

以前主要以风洞试验为主要研究手段。在研究风荷载作用下的大跨度桥梁的气动稳定性时,经常假设来风的方向与桥跨正交时是最不利的。

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18、

Also, spin rate coupling with structural damping ratio and other structural parameters have a significant influence in aeroelastic dynamic instability for spinning rocket.

旋转速率与结构阻尼及其他结构参数对气动弹性动态稳定性影响也比较显著。

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19、

wind tunnel test on an aeroelastic model of grandstand cantilevered roof of large stadium and features of wind-induced response

体育场主看台弧形挑篷气弹模型风洞试验和响应特性

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20、

an analysis method of static aeroelastic characteristics of supercritical wing

超临界机翼静气动弹性特性研究

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