The probe has been successfully used for measuring rotating stall signals of a single stage transonic compressor.
用该探针成功地测出了一台跨音速单级轴流压气机的旋转失速信号。
Experimental results show a promising prospect for utilizing the injector driven technique in advanced transonic wind tunnels.
实验研究还表明引射驱动方式应用于跨音速风洞具有光明的前景。
Empirical results are needed in the transonic Mach regime.
在跨音速马赫数范围内需要经验结果。
Numerical simulation of viscous flows through multistage transonic fans was carried out.
进行了多级跨音速风扇粘性流动的数值模拟研究。
An implicit time-marching method is presented for solving the transonic Euler equations.
本文提出了求解跨音速欧拉方程的一种隐式时间推进法。
An iteration method is used for computing the transonic pressure distribution on a flexible wing.
本文采用迭代求解的方法计算弹性机翼的跨音速压强分布。
Flapping and rotary gap have been investigated with the help of transonic unsteady aerodynamic forces.
使用跨音速非定常空气动力，对扑动间隙和旋转间隙进行研究。
Coupled with the structural equations, the models for transonic aeroelasticity in state-space are got.
耦合结构动力学方程，建立了基于状态空间的跨声速气动弹性分析模型。
An arbitrary airfoils blade design procedure was adopted to redesign a transonic fan with compound swept.
采用任意中弧线叶片造型程序，将某单级跨声、常规设计的风扇改进为复合掠形设计。
Computation of wing flutter for unsteady transonic flows in the frequency domain is studied in this thesis.
本文研究了机翼跨音速颤振的频域计算方法。
Several computed results of transonic turbine cascades are presented to illustrate the method's capabilities.
为论证方法的有效性，给出了几个跨音速涡轮叶栅的计算结果。
A finite difference method for computing the axisymmetric, transonic flows over nacelle is presented in this paper.
本文考虑轴对称跨音速进气道外流场的有限差分计算方法。
This paper represents a CFD method for the design of NLF airfoils directly under transonic viscous flow conditions.
本文介绍一种设计跨声速自然层流翼型的计算流体力学（CFD）方法。
Numerical analyses of the transonic nozzle inviscid flow and supersonic jet impingement on a jet TAB are presented.
采用数值分析方法分析了跨声速喷管无粘流动和超声速射流对挡流板的冲击流场。
This paper is a report of experimental pressure. Measurement research for NACA0012 airfoil in NH-1 transonic wind tunnel.
本文为NACA0012翼型在NH - 1风洞进行跨音速二维测压实验的研究报告。
The paper presents some research works on the internal flow shock wave measurement of transonic compressor by PIV technique.
在跨音压气机试验台上进行了用PIV技术测量内流激波结构的试验研究。
A numerical method is presented for predicting unsteady transonic aerodynamic flow about aircraft wings with control surface.
本文介绍一种带操纵面机翼的非定常跨声速流的有限差分计算方法。
This paper deals with the inverse design problem of transonic turbine cascade in the hodograph plane by the finite area method.
本文给出了基于有限面积法的跨音速透平叶栅速度面反问题设计方法。
The conservative full potential equation and C H grid are used to compute the unsteady transonic flows around airfoils and wings.
采用C-H型网格、守恒型非定常全位势方程的时间精确近似因式分解差分法计算二维、三维的跨声速非定常位势流。
In this paper the Direct Iterative Surface Curvature (DISC) design method is presented for designing airfoils at transonic speeds.
本论文采用直接表面曲率迭代方法(DISC)进行跨声速翼型设计。
But the aerodynamic optimization of the turbomachinery blade, especially the transonic compressor blade, is still a challenge area.
但是叶轮机械，尤其是跨音速轴流压气机叶片的气动优化设计仍然是一个具有挑战性的研究领域。
Using the improved method we studied inviscid and viscous transonic flow in turbomachinery based on Euler and Navier Stokes equations.
计算结果表明，本方法是透平机械内部跨音速流动计算的强有力的手段。
The new method is used to study transonic flow in cascades and one kind of complex unsteady transonic axisymmetric flow in arc breaker.
利用本文的方法，分别计算了跨声速叶栅流动和工程中一类复杂非定常轴对称跨声速流动。
A kernel function method and the results of computing unsteady load on three-dimensional wings in transonic flow are presented in this paper.
本文给出了在跨音速流动中，计算三维机翼非定常载荷分布的核函数法和计算结果。
The variation finite element method (FEM) using the pseudo-potential function was presented for the simulation of transonic rotational flows.
本文运用赝势函数变分有限元方法数值模拟了绕翼型的跨音速有旋流动。
The effect of acoustic excitation on the flow asymmetry over a slender body in compressible flows was investigated in a transonic wind tunnel.
在跨声速风洞中研究了声激励对于可压缩流中细长旋成体大迎角流动非对称性的影响效果。
This paper describes the initial experimental results of aeroelastic instability of BF-1 rotors on a transonic axial compressor facility at BIAA.
本文介绍了在跨音压气机试验台上对BF - 1系列转子开展气动弹性失稳的实验研究工作。
Using the above method, numerical simulations are implemented for supersonic, transonic and subsonic flows around three-dimensional open cavities.
运用此方法，本文数值模拟了三维开式空腔的超声速、跨声速、亚声速流动。
Using the above method, numerical simulations are implemented for supersonic, transonic and subsonic flows around three-dimensional open cavities.
运用此方法，本文数值模拟了三维开式空腔的超声速、跨声速、亚声速流动。
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