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Browse our Compressors Publications
Read the latest and previous editions of our publications on Compressors in our library
Redesign of Transonic Compressor using 3D Inverse Design
This paper presents the redesign of a transonic rotor performed by means of a 3D viscous inverse design method.
On 3D Inverse Design of Centrifugal Compressor Impellers with Splitter Blades
In the design of centrifugal compressor impellers with splitter blades it is quite common to use the same blade shapes on the full and splitter blades with the splitters placed at the mid-pitch location.
Aerodynamic and Aeroacoustic Optimization of a Transonic Centrifugal Compressor
The performance of transonic compressors can be characterized aerodynamically and aeroacoustically. In this paper, the DLR SRV2 compressor without vaned diffusers and its redesigned version are studied.
Numerical Prediction of the Aerodynamic Noise Generated by a Supersonic Centrifugal Compressor
This paper presents a numerical study of predicting the aerodynamic noise generated by a supersonic centrifugal compressor, which can advance the understanding of noise generation mechanisms so that future optimization can be done to achieve a better design.
Optimization of 6.2:1 Pressure Ratio Centrifugal Compressor Impeller by 3D Inverse Design
In this work, the redesign of a centrifugal transonic compressor impeller with splitter blades by means of the three-dimensional inverse design code TURBOdesign-1 is presented.
Development of a High Performance Centrifugal Compressor Using a 3D Inverse Design Technique
Diesel engines developed to meet future US and European emissions regulations place an unprecedented demand on compressor performance in terms of pressure ratio and flow range capability.
Investigation of an Inversely Designed Centrifugal Compressor Stage - Part I: Design and Numerical Verification
In this paper the three-dimensional inverse design code TURBOdesign-1 is applied to the design of the blade geometry of a centrifugal compressor impeller with splitter blades.
Optimization of Microturbine Aerodynamics Using CFD, Inverse Design and FEM Structural Analysis (1st Report: Compressor Design)
In this paper, a new aerodynamic design procedure is presented for a centrifugal compressor stage of a microturbine system.
Investigation of an Inversely Designed Centrifugal Compressor Stage - Part II: Experimental Investigations
This paper presents an experimental investigation of two centrifugal compressor stage configurations. The baseline configuration has been designed using conventional design engineering tools.
