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Numerical Investigation of a Transonic Centrifugal Compressor

Journal of Turbomachinery, 2006
A three-dimensional Navier-Stokes solver is used to investigate the flow field of a high-pressure ratio centrifugal compressor for turbocharger applications. Such a compressor consists of a double-splitter impeller followed by a vaned diffuser. The inlet flow to the open shrouded impeller is transonic, thus giving rise to interactions between shock ...
MARCONCINI, MICHELE   +3 more
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The J83 Seven-Stage Transonic Compressor

Journal of Engineering for Power, 1961
The J83 turbojet engine was a high-performance, lightweight engine with a maximum thrust of 2450 lb, a diameter of 18 in., and a weight of approximately 300 lb. The compressor for this engine was a seven-stage, transonic, axial-flow compressor with an inlet tip diameter of 15.2 in. and a hub-lip ratio of 0.433.
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Understanding Unsteady Flow Features in Transonic Compressors

Computing in Science & Engineering, 2007
Applying computational science and engineering to the design and analysis of high-performance compressors makes it possible to understand unsteady flow effects in gas turbine engines. Simulations have produced numerical data of greatly improved geometric, physical, and numerical fidelity than previously possible, helping next-generation engines achieve
Steven E. Gorrell   +2 more
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Approach to High Performance Transonic Centrifugal Compressor

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2002
A single stage transonic centrifugal compressor for a small turbofan engine has been developed. Rig testing has demonstrated 83.2 percents of adiabatic efficiency for 7.5:1 of total to static pressure ratio, using a corrected tip speed of 596 m/sec. This paper mainly presents an impeller blade redesign approach from original blade geometry, based on ...
Mineyasu Oana   +3 more
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Experimental Investigation of a Transonic Aspirated Compressor

Journal of Turbomachinery, 2003
Abstract The experimental investigation of a transonic aspirated stage demonstrating the application of boundary layer aspiration to increase stage work is presented. The stage was designed to produce a pressure ratio of 1.6 at a tip speed of 750ft∕s resulting in a stage work coefficient of 0.88.
Brian J. Schuler   +2 more
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Simulation of transonic flow in radial compressors

Computer Methods in Applied Mechanics and Engineering, 1987
Abstract A collection of computer codes for the generation of grids and the solution of the Euler equations have been developed for the purpose of simulating the complex three-dimensional transonic and rotational flow through high pressure ratio radial compressors.
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Reverse engineering EEE transonic compressor fan blade

AIAA SCITECH 2023 Forum, 2023
Bharadwaj Dogga, Mark G. Turner
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Development of a Transonic Compressor Test Facility

2008
PROCEEDINGS OF THE ECOS2008, 21ST INTERNATIONAL CONFERENCE ON EFFICIENCY, COST, OPTIMIZATION, SIMULATION AND ENVIRONMENTAL IMPACT OF ENERGY SYSTEMS, JUNE 24 – 27, 2008, KRAKÓW, POLAND.
BIOLLO, ROBERTO, BENINI, ERNESTO
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