On the Design of a Multi-Megawatt Oil-Free Centrifugal Compressor for Supercritical Speeds, ASME-IMECE, Vancouver BC, Canada, November 2010,
Evaluating Complex Inlet Distortion With a Parallel Compressor Model: Part 1 Proceedings of ASME Turbo Expo 2011, 6-10 June 2011, Vancouver, Canada,
Experimental and Numerical Investigation of Tip Clearance and Bleed Effects in a Centrifugal Compressor Stage With Pipe Diffuser on ResearchGate, the o
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Operability Using a Modified Parallel Compressor gathered at the United States Air Force Academy.rence and Exposition, Vancouver, Canada, (2011)
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Development of Water Lubricated Compressor-Expander for Fuel Cell ApplicationVancouver. British Columbia, Canada: ASME, 2010 :875 - 881
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Aerodynamic Optimisation of a Centrifugal Compressor Return Channel and U-Turn With Genetic Algorithms on ResearchGate, the professional network for scientist
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Investigations of Secondary Flow Suction in a High Speed Compressor Cascade.In: Proceedings of the ASME Turbo Expo 2011, Vancouver, Canada (2011)
Aerodynamic Forcing Part I:Highly Loaded Transonic Compressor[R].ASME GT2010Proceedings of the ASME Turbo Expo 2011, Vancouver, CanadaFruth, F., Vogt
Publication » Effects of Inlet Flow Field Conditions on the Performance of Centrifugal Compressor Diffusers: Part 2—Straight-Channel Diffuser. Compressor
Optimization of 6.2:1 Pressure Ratio Centrifugal Compressor Impeller by 3D ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, Vancouver,
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