The inherency frequency and vibratory-type are calculated based on the modal analysis of the whole airframe.

对机身整框架进模态分析,求解固有频率和振型。

The multidimensional modal theory is applied to solve liquid nonlinear sloshing in right circular cylindrical tank in translatory motion.

将多维模态理论应用到求解作横向运动圆柱贮箱中液线性晃动问题。

Message boxes are usually run modally: the question must be answered before the program may continue.

消息框通常模态运：即走程序继续运须回答问题。

From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.

摘要根据热气动弹性特点，探讨了气动加热温度对三角机翼模态特性和颤振特性影响。

The inherency frequency and vibratory-type are calculated based on the modal analysis of the whole airframe.

对机身整体框架进行分析,求解固有频率和振型。

The multidimensional modal theory is applied to solve liquid nonlinear sloshing in right circular cylindrical tank in translatory motion.

将多维理论应用到求解作横向运动圆柱贮箱中液体的非线性晃动问题。

Message boxes are usually run modally: the question must be answered before the program may continue.

消息框运行：即走程序继续运行前必须回答问题。

From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.

摘要根据热气动弹性特点，探讨了气动加热温度对三角机翼特性和颤振特性的影响。

The inherency frequency and vibratory-type are calculated based on the modal analysis of the whole airframe.

对机身整体框架进行模态分析,求解固有频率和振型。

The multidimensional modal theory is applied to solve liquid nonlinear sloshing in right circular cylindrical tank in translatory motion.

将多维模态理论应用到求解作横向运动圆柱液体的非线性晃动题。

Message boxes are usually run modally: the question must be answered before the program may continue.

消息框通常模态运行：即走程序继续运行前必须题。

From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.

摘要根据热气动弹性特点，探讨了气动加热温度对三角机翼模态特性和颤振特性的影响。

The inherency frequency and vibratory-type are calculated based on the modal analysis of the whole airframe.

对机身整体框架进行模态分析,求解固有频率和振型。

The multidimensional modal theory is applied to solve liquid nonlinear sloshing in right circular cylindrical tank in translatory motion.

将多维模态用到求解作横向运动圆柱贮箱中液体的非线性晃动问题。

Message boxes are usually run modally: the question must be answered before the program may continue.

消息框通常模态运行：即走程序继续运行前必须回答问题。

From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.

摘要根据热气动弹性特，了气动加热温度对三角机翼模态特性和颤振特性的影响。

The inherency frequency and vibratory-type are calculated based on the modal analysis of the whole airframe.

对机身整体框架进行模态分析,求解固有频率和振型。

The multidimensional modal theory is applied to solve liquid nonlinear sloshing in right circular cylindrical tank in translatory motion.

将多维模态理论应用到求解作横向运动圆柱贮箱中液体的非线性晃动问题。

Message boxes are usually run modally: the question must be answered before the program may continue.

消息框通常模态运行：即走程序继续运行前必须回答问题。

From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.

摘要根据热气动弹性特点，探讨了气动加热温度对三角机翼模态特性和颤振特性的影响。

The inherency frequency and vibratory-type are calculated based on the modal analysis of the whole airframe.

对机身整体框架进行模态分析,求解固有频率和振型。

The multidimensional modal theory is applied to solve liquid nonlinear sloshing in right circular cylindrical tank in translatory motion.

将多维模态理论应用到求解作横向运动圆柱贮箱中液体的非线性晃动问题。

Message boxes are usually run modally: the question must be answered before the program may continue.

消息框通常模态运行：即走程序继续运行前必须回答问题。

From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.

摘要根据热气动弹性特点，探讨了气动加热温度对三角机翼模态特性和颤振特性的影响。

The inherency frequency and vibratory-type are calculated based on the modal analysis of the whole airframe.

对机身整体框架进行模态分析,解固有频率和振型。

The multidimensional modal theory is applied to solve liquid nonlinear sloshing in right circular cylindrical tank in translatory motion.

将多维模态理论应解作横向运动圆柱贮箱中液体的非线晃动问题。

Message boxes are usually run modally: the question must be answered before the program may continue.

消息框通常模态运行：即走程序继续运行前必须回答问题。

From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.

摘要根据热气动点，探讨了气动加热温度对三角机翼模态和颤振的影响。

The inherency frequency and vibratory-type are calculated based on the modal analysis of the whole airframe.

对机身整体框架进行模态分析,求解固有频率和振型。

The multidimensional modal theory is applied to solve liquid nonlinear sloshing in right circular cylindrical tank in translatory motion.

将多维模态理论应用到求解作横向运动圆柱贮箱中液体的非线性晃动问题。

Message boxes are usually run modally: the question must be answered before the program may continue.

消息框通常模态运行：即走程序继续运行前必须回答问题。

From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.

摘要根据热气动弹性特点，探讨了气动加热温度对三角机翼模态特性和颤振特性的影响。

The inherency frequency and vibratory-type are calculated based on the modal analysis of the whole airframe.

机身整体框架进行模态分析,求解固有频型。

The multidimensional modal theory is applied to solve liquid nonlinear sloshing in right circular cylindrical tank in translatory motion.

将多维模态理论应用到求解作横向运动圆柱贮箱中液体的非线性晃动问题。

Message boxes are usually run modally: the question must be answered before the program may continue.

消息框通常模态运行：即走程序继续运行前必须回答问题。

From the characteristics of aerothermoelasticity, the effects of temperature in aerodynamic heating on the mode of a delta wing and the characteristic of its flutter were researched.

摘要根据热气动弹性特点，探讨了气动加热温角机翼模态特性颤特性的影响。