Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel

Widen Tabakoff,; Robert Mason,

doi:10.1515/TJJ.2007.24.2.85

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Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel

Widen Tabakoff, and Robert Mason,

Published/Copyright: June 1, 2007

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From the journal International Journal of Turbo and Jet Engines Volume 24 Issue 2

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Vancouver

Tabakoff,, Widen and Mason,, Robert. "Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel" International Journal of Turbo and Jet Engines, vol. 24, no. 2, pp. 85-92. https://doi.org/10.1515/TJJ.2007.24.2.85

Tabakoff,, W. & Mason,, R. (). Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel. International Journal of Turbo and Jet Engines, 24(2), 85-92. https://doi.org/10.1515/TJJ.2007.24.2.85

Tabakoff,, W. and Mason,, R. () Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel. International Journal of Turbo and Jet Engines, Vol. 24 (Issue 2), pp. 85-92. https://doi.org/10.1515/TJJ.2007.24.2.85

Tabakoff,, Widen and Mason,, Robert. "Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel" International Journal of Turbo and Jet Engines 24, no. 2 (): 85-92. https://doi.org/10.1515/TJJ.2007.24.2.85

Tabakoff, W, Mason, R. Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel. International Journal of Turbo and Jet Engines. ;24(2): 85-92. https://doi.org/10.1515/TJJ.2007.24.2.85

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Published Online: 2007-06

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Articles in the same Issue

CONTENTS
Experimental Studies on Hydrodynamics of Recirculating Fluidized Beds
Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel
Numerical Simulation of Plane Mixing Layer by Three-Dimensional Vortex Method
Performance Prediction of Subsonic Vaned Diffusers Using an Integral Boundary Layer Method
Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours
A Contribution to the Analysis of the Performance of the Gas Turbine Using Simulation
Numerical Studies of a Novel Vortex Combustor

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https://doi.org/10.1515/TJJ.2007.24.2.85

Articles in the same Issue

CONTENTS
Experimental Studies on Hydrodynamics of Recirculating Fluidized Beds
Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel
Numerical Simulation of Plane Mixing Layer by Three-Dimensional Vortex Method
Performance Prediction of Subsonic Vaned Diffusers Using an Integral Boundary Layer Method
Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours
A Contribution to the Analysis of the Performance of the Gas Turbine Using Simulation
Numerical Studies of a Novel Vortex Combustor