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. LohSpringer Berlin Heidelberg
AXIAL FLOW FAN DESIGN 热度: USER MANUAL 3_2.1.X AXIAL TURBINE FLOW PATH DESIGN_E1-2 热度: Brochure Moreinformationfromhttp://.researchandmarkets/reports/2179343/ AxialFlowCompressors.AStrategyforAerodynamicDesignandAnalysis Description:Thisexcitingnewtextprovidesathoroughdescriptionofanaerodynamicdesignandanal...
This paper presents results of aerodynamic enhancement of axial compressors utilizing optimum natural aspiration through a circumferential slot made within the casing wall upstream the rotor blades row. The method of investigation is based on numerical simulation of flow field. Geometries of the slot wal...
The development of design techniques for turbomachinery profiles has been a relevant research area for the last 50 years, for application in propulsion and energy systems. Different approaches have emerged between turbines and compressors, between axial and radial machines, and between compressible and ...
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Design of centrifugal compressors for heat pump systems 2018, Applied Energy Show abstract Design point optimization of an axial-flow compressor stage 1989, International Journal of Heat and Fluid Flow Show abstract Aerodynamic preliminary design optimization of a centrifugal compressor turbocharger based ...
• AXCOM: an aerodynamic performance analysis for single-stage or multistage axial-flow compressors. • AXSTAGE: an axial-flow compressor stage design program. • AXDESIGN: a multistage axial-flow compressor design program. • EXHAUST: an exhaust diffuser aerodynamic performance analysis (includ...
the complex shock waves in the cascade channel also bring more aerodynamic losses. This paper proposes a supersonic compressor cascade modeling method based on the theory of unique inlet flow angle, and the aerodynamic design and optimization of a cascade with inlet Mach number 1.85 are studied by...
Highly loaded axial flow compressor history and current development Journal of Turbomachinery, 112 (4) (1990), pp. 567-578 Google Scholar 2 Loughery R, Horn R A. Single stage experimental evaluation of boundary layer blowing and bleed techniques for high lift stator blades. NASA CR-54573, 1971...