Numerical investigation & comparison of a tandem-bladed turbocharger centrifugal compressor stage with conventional design

Author:

Danish Syed Noman,Qureshi Shafiq Rehman,EL-Leathy Abdelrahman,Khan Salah Ud-Din,Umer Usama,Ma Chaochen

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference21 articles.

1. Rodgers C., Unusual Centrifugal Compressors and Applications. AIAA-95-2346, 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exibit, San Diego, July 10–12, 1995

2. Klassen H. A., Wood J. R., Schumann L. F., Experimental performance of a 13.65-centimeter-tip-diameter tandem-bladed sweptback centrifugal compressor designed for a pressure ratio of 6. NASA Center for Aero-Space Information (CASI) NASA-TP-1091, 19771101, 1977

3. Young M. Y., Struble A. G., Compressor Impeller with Displaced Splitter Blades, US Patent 5,002,461, 1991

4. Bache G., Impeller Tandem Blade Study With Grid Embedding for Logical Grid Refinement. Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, April 28–30, 1992, Huntsville, Alabama, USA, NASA Conference Publication 3163, Part 1

5. Josuhn-Kadner B. and Hoffmann B., Investigations on a Radial Compressor Tandem-Rotor Stage With Adjustable Geometry. 37th ASME International Gas Turbine and Aeroengine Congress and Exposition, 1–4 June 1992, Cologne, Germany, ASME Paper 92-GT-218

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