The Effects of Reynolds Number on the Efficiency of Centrifugal Compressor Stages An analysis of the friction losses in a centrifugal compressor stage is used to suggest a new form of correction equation for the effect of Reynolds number... MV Casey - 《Journal of Engineering for Gas Turbines ...
The evolution of the impact force, energy absorption, temperature rise and the crack propagation are analyzed. It is worth mentioning that the thermal/aerodynamic effects on the casing containment may be also important, especially for the high-pressure compressor casing. In the current study, the ...
Structural parameter effect of a railway hydraulic damper on its dynamic damping characteristics A parametric dynamic damping characteristics model, which includes the dynamic force equilibrium equation, the flow continuity equation, the flow losses model, the comprehensive stiffness model and the valve dyna...
Riccati equationimpedance matrixmodal scattering propertiesThe paper is concerned with the measurement of the random pressure fluctuations on the rotating blades of a low pressure axial fan. The force fluctuations due to the pressure fluctuations are the d...
Leading Edge Thicker portion of the airfoil that is the first part of the blade to meet the air. Net Free Area Net area at the plane of the fan through which all air must pass. Usually based on the nominal fan diameter minus seal disc area or hub diameter. Note that blade area is ...
Through the radial momentum equation, this radial force variation is responsible for creating the streamline curvature that leads to the expansion of the streamtube (slipstream) that is responsible for slowing the wind velocity ahead of the wind turbine leading edge, which is quantified as the ...
Through the radial momentum equation, this radial force variation is responsible for creating the streamline curvature that leads to the expansion of the streamtube (slipstream) that is responsible for slowing the wind velocity ahead of the wind turbine leading edge, which is quantified as the ...
axial force testing and validation experiments on the torque converter prototype have been completed. The research findings reveal that changes in oil viscosity resulting from variations in charging oil temperature have a considerable impact on the axial force of the torque converter. The axial force ...
Inspired by this, bionic design of two-stage fan blades was carried out by applying only a certain range of wing angle structure on the blade without changing the parameters of the prototype blade, such as airfoil, twist angle α and blade height H, as shown in Figure 5. The wing angle...
A one equation turbulence model for aerodynamic flows. Rech. Aerosp. 1994, 1, 5–21. [Google Scholar] © 2016 by the authors; licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC-BY) ...