Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor

S. Jonnavithula,; F. Sisto,; S. Thangam,

doi:10.1515/TJJ.1992.9.1.49

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Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor

S. Jonnavithula, , F. Sisto, and S. Thangam,

Published/Copyright: March 1, 1992

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From the journal International Journal of Turbo and Jet Engines Volume 9 Issue 1

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Jonnavithula,, S., Sisto,, F. and Thangam,, S.. "Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor" International Journal of Turbo and Jet Engines, vol. 9, no. 1, 1992, pp. 49-66. https://doi.org/10.1515/TJJ.1992.9.1.49

Jonnavithula,, S., Sisto,, F. & Thangam,, S. (1992). Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor. International Journal of Turbo and Jet Engines, 9(1), 49-66. https://doi.org/10.1515/TJJ.1992.9.1.49

Jonnavithula,, S., Sisto,, F. and Thangam,, S. (1992) Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor. International Journal of Turbo and Jet Engines, Vol. 9 (Issue 1), pp. 49-66. https://doi.org/10.1515/TJJ.1992.9.1.49

Jonnavithula,, S., Sisto,, F. and Thangam,, S.. "Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor" International Journal of Turbo and Jet Engines 9, no. 1 (1992): 49-66. https://doi.org/10.1515/TJJ.1992.9.1.49

Jonnavithula, S, Sisto, F, Thangam, S. Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor. International Journal of Turbo and Jet Engines. 1992;9(1): 49-66. https://doi.org/10.1515/TJJ.1992.9.1.49

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Published Online: 1992-03

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Articles in the same Issue

CONTENTS
Basic Analysis of Counter-Rotating Turbines
Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
Fighter Aircraft Affordability, Survivability, and Effectiveness Through Multi-Function Thrust-Vectoring Nozzles
Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor
Influences of Inlet Conditions on Flow Distortion in a Circular-to-Rectangular Transition Duct

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https://doi.org/10.1515/TJJ.1992.9.1.49

Articles in the same Issue

CONTENTS
Basic Analysis of Counter-Rotating Turbines
Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
Fighter Aircraft Affordability, Survivability, and Effectiveness Through Multi-Function Thrust-Vectoring Nozzles
Experienced Investigation of Rotating Stall in a Single-Stage Axial Compressor
Influences of Inlet Conditions on Flow Distortion in a Circular-to-Rectangular Transition Duct