1、

High temperature and high expansion ratio lead to local transonic in the turbine.

高温、高膨胀比必然带来涡轮内部流动的局部超声速。

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2、

Full 3D iterative solution of transonic flow for a swept wing test channel

后掠冀跨声流场S1/S2流面全三元迭代解

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3、

Preliminary PIV Measurement of Unsteady Tip Flow in a Transonic Fan Rotor

跨音风扇转子尖部非定常流场的PIV初步测量

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4、

Subsonic and transonic wing inverse design using control theory

亚、跨音速三维机翼气动外形反设计的控制理论方法

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5、

The Transonic Integral Equation of Three Dimensional Thin Wing and the Solutions of Finite Element Method

三维薄翼跨音速积分方程及其有限元解法

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7、

In this paper, the transonic two dimensional airfoil integral equation given by Nixon [ 1,2,3] has been extended to three dimensional thin wing case.

本文将Nixon[1,2,3]对二维薄翼型所建立的跨音速积分方程推广到三维薄机翼情况。

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8、

Theory, method and application of three-dimensional flow design of transonic axial-flow compressors

跨声速轴流式压气机三元流动设计的理论、方法和应用

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9、

AN INVERSE DESIGN METHOD OF TRANSONIC AIRFOIL AND WING A Mass Addition Approach to the Bypass Turbomachine Through Flow Inverse Design Problem

跨音速翼型和机翼的反设计计算方法双函道叶轮机通流反问题的加质量法

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10、

Transonic tube wind tunnel flows over supercritical airfoils with slots on both upper and lower walls have been simulated by using compressible unsteady two dimensional Navier-Stokes equations.

本文采用二维可压缩非定常N-S方程模拟了带有上下开槽壁的跨声速二维管风洞中超临界翼型绕流的流场。

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11、

Transonic vibration induced by mismatching between engine and thrust nozzle

发动机和尾喷管匹配引起的跨音振动

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12、

A Numerical Experiment in Computation of Transonic Cascade by Time-Dependent Method

用时间相关法计算跨音速叶栅的数值试验

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13、

The time-dependent method is applied to the calculation of transonic nozzle flow in this paper.

本文用时间相关法求解定常跨声速喷管流场。

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14、

A computational program for solving the transonic flow field through plane cascades by a time-dependent method

求解平面叶栅跨音流场的一个时间相关法计算程序

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15、

The computation of transonic nozzle flow-field by a time-dependent method

用时间相关法计算喷管跨声速流场

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16、

In this paper, the time-dependent method is applied to the numerical computation of transonic nozzle flows by using of conservation and nonconservation governing equations.

用时间相关法数值计算跨音速喷管流动时,其控制方程分别采用守恒型和非守恒型方程。

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17、

Application of the time-dependent finite-volume method to the calculation of transonic cascade flow field

时间相关有限体积法在跨音速叶栅流场计算上的应用

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18、

A CRYOGENIC HIGH-REYNOLDS NUMBER TRANSONIC WIND TUNNEL WITH PRE-COOLED AND RESTRICTED FLOW The Effects of Tip End Ejection Area Ratio and Installation Angle on Heat Transfer of Orthogonally Rotating Rectangular Duct with Staggered Pin Fins

预冷节流式暂冲高雷诺数低温空气跨声速风洞方案正交旋转径向出流带扰流柱的矩形通道出口节流及安装角对传热的影响

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19、

Study of the Impact of Afterbody Shape on Weathercock Stability for Transonic Transport Airplane

跨音速运输机机身后体对航向静稳定性影响研究

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20、

It can insulate the upstream and downstream flow field resulting in the noise drop of the text section from the downstream and can control the Mach number exactly in the transonic state.

它在跨声速状态下具有隔离上下游流场从而降低试验段噪声,精确控制马赫数的作用。

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