This webinar presents the redesign of an electrically driven mixed flow transonic compressor by using a 3D inverse design methodology. The compressor will be used for an active high-lift system application that aims to delay the onset of stall and thus contributing to the reduction of both the aircraft noise footprint and the impact of aviation emission on local air quality.
In this webinar we will show how the newly developed meanline design code for Francis turbine, which has been recently developed in TURBOdesign Suite, can be used to do the initial sizing of all components of a Francis turbine from volute, stay vane, guide vane and runner.
In this webinar, you will learn how to approach the design of high performance hydrogen compressor and pump and discover how TURBOdesign Suite combined with Ansys Workbench can be used to design these turbomachinery components.
The design of waste water pumps requires complicated trade-off between non-clogging characteristic of the impeller with its efficiency and cavitation performance. In this webinar, we will show an automated process for optimizing the design of waste water pumps by using 3D inverse design method.
This webinar present a rapid and efficient design and optimization process for axial contra-rotating fans. The speakers - Prof. Mehrdad Zangeneh, Saurabh Gupta and Tobis Sieger - present application of TURBOdesign tools for the preliminary multi-blade row design of the axial fan where the rpm and pressure rise repartition of the different stages are varied.
Playback to see how the performance of an Axial and Centrifugal Fan can be optimized for improved stage performance by using the inverse design method. We will demonstrate how the efficient optimization methods within TURBOdesign Suite allow designers to produce high performance, optimized designs within industrial timescales.
This webinar will present a rapid and efficient design and optimization process for axial contra-rotating fans. The speakers will present application of TURBOdesign tools for the preliminary multi-blade row design of the axial fan where the rpm and pressure rise repartition of the different stages are varied.
The aerodynamic optimization of centrifugal compressors requires better understanding of different sources of loss. In this webinar, we will use entropy production rate to distinguish the different sources of loss in a subsonic and a transonic centrifugal compressor impeller under different operating conditions.