Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response

J.R. Fagan,; S. Fleeter,

doi:10.1515/TJJ.1992.9.3.191

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Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response

Published/Copyright: September 1, 1992

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From the journal International Journal of Turbo and Jet Engines Volume 9 Issue 3

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Harvard
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Vancouver

Fagan,, J.R. and Fleeter,, S.. "Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response" International Journal of Turbo and Jet Engines, vol. 9, no. 3, pp. 191-204. https://doi.org/10.1515/TJJ.1992.9.3.191

Fagan,, J. & Fleeter,, S. (). Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response. International Journal of Turbo and Jet Engines, 9(3), 191-204. https://doi.org/10.1515/TJJ.1992.9.3.191

Fagan,, J. and Fleeter,, S. () Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response. International Journal of Turbo and Jet Engines, Vol. 9 (Issue 3), pp. 191-204. https://doi.org/10.1515/TJJ.1992.9.3.191

Fagan,, J.R. and Fleeter,, S.. "Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response" International Journal of Turbo and Jet Engines 9, no. 3 (): 191-204. https://doi.org/10.1515/TJJ.1992.9.3.191

Fagan, J, Fleeter, S. Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response. International Journal of Turbo and Jet Engines. ;9(3): 191-204. https://doi.org/10.1515/TJJ.1992.9.3.191

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Articles in the same Issue

CONTENTS
Three-Dimensional Viscous Flow Through a Highly Loaded Compressor Rotor
Studies on the Effect of Turbulence on the Spreading Rates of Bluff-Body Stabilized Flames
Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response
Semi-Analytical Fuel Injector Performance Correlation Approach
Numerical Flow Analysis in Modern Gas Turbine Design
Examination of Interactions Between Turbulence and Combustion in Diffusion Flame
Three-Dimensional Incompressible Flow Solution of an Axial Compressor Using Pseudostream-Functions Formulation

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https://doi.org/10.1515/TJJ.1992.9.3.191

Articles in the same Issue

CONTENTS
Three-Dimensional Viscous Flow Through a Highly Loaded Compressor Rotor
Studies on the Effect of Turbulence on the Spreading Rates of Bluff-Body Stabilized Flames
Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response
Semi-Analytical Fuel Injector Performance Correlation Approach
Numerical Flow Analysis in Modern Gas Turbine Design
Examination of Interactions Between Turbulence and Combustion in Diffusion Flame
Three-Dimensional Incompressible Flow Solution of an Axial Compressor Using Pseudostream-Functions Formulation