Fundamental aerothermodynamic equations derived in Chapter 1 may now be applied for aerodynamic design of axial flow compressors and turbines. A typical sketch of an axial flow compressor is shown in Fig. 3-1.doi:10.1007/978-3-642-46109-5_3W. H. T. Loh...
Aerodynamic design of axial-flow compressors prepared by members of the staff of Lewis Reserch Center, [NASA] Cleveland, Ohio ; edited by Irving A. Johnsen and Robert O. Bullock (NASA SP, 36) Scientific and Technical Information Division, National Aeronautics and Space Administration, 1965 Revise...
BrochureMoreinformationfromhttp://.researchandmarkets/reports/2179343/AxialFlowCompressors.AStrategyforAerodynamicDesignandAnalysisDescription:This excitingnewtext providesathoroughdescriptionofanaerodynamicdesignandanalysissystemforaxial–flowcompressors.Itdescribesthebasicfluiddynamicandthermodynamicprinciples,empiricalmodels...
This paper summarizes the state of 3D CFD based models of the time-averaged flow field within axial flow multistage turbomachines. Emphasis is placed on models that are compatible with the industrial design environment and those models that offer the potential of providing credible results at both ...
Aerodynamic Design Aspects for Stator of Highly Loaded Tandem Bladed Axial Compressor Tandem bladed axial compressors prove to be a promising way of increasing the total pressure rise capability per stage with acceptable losses. The practica... A Singh,CS Mistry - 《Volumea Turbomachinery》 被引量...
The choice of the stator hub configuration (i.e. cantilevered versus shrouded) is an important design decision in the preliminary design stage of an axial compressor. Therefore, it is important to understand the effect of the stator hub configuration on the aerodynamic performance. In particular, ...
A stage-by-stage simulation method is introduced for analysis of inlet total pressure distortion effect on the multistage axial flow compressor characteris... C Rui - 《Aeroengine》 被引量: 4发表: 2007年 A theoretical treatment of technical risk in modern propulsion system design All three are...
3.Finally,it is suggested that the flying wing configuration is an optimal selection of aerodynamic configuration design of an UCAV for reconnaissance.最后,指出飞翼布局是无人侦察作战飞机气动布局的较好选择。 英文短句/例句 1.A Study of New Type Configuration of Blade Cascade in Axial Compressors;轴流...
3.The paper specifies the engineering method for aerodynamic design of counter rotating axial-flow fan, that is criterion optimization method.论述了对旋式轴流通风机气动设计的工程方法——判据优化法;给出了设计计算的主要关系式;阐述了设计计算应遵循的原则、方法和步骤;以№14矿用对旋式主轴流通风机为例...
An overall blockage attenuation-based aerodynamic performance and stability design optimization method for transonic axial flow compressors PurposeThis study aims to use computational fluid dynamics (CFD) to understand and quantify the overall blockage within a transonic axial flow compressor (... X Wang...