Probabilistic Finite Element Analysis of a Non-Gasketed Flange

Rama Subba Reddy Gorla,; Sreekantha Reddy Gorla,

doi:10.1515/TJJ.2007.24.1.51

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Probabilistic Finite Element Analysis of a Non-Gasketed Flange

Rama Subba Reddy Gorla, and Sreekantha Reddy Gorla,

Published/Copyright: March 1, 2007

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From the journal International Journal of Turbo and Jet Engines Volume 24 Issue 1

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Gorla,, Rama Subba Reddy and Gorla,, Sreekantha Reddy. "Probabilistic Finite Element Analysis of a Non-Gasketed Flange" International Journal of Turbo and Jet Engines, vol. 24, no. 1, pp. 51-62. https://doi.org/10.1515/TJJ.2007.24.1.51

Gorla,, R. & Gorla,, S. (). Probabilistic Finite Element Analysis of a Non-Gasketed Flange. International Journal of Turbo and Jet Engines, 24(1), 51-62. https://doi.org/10.1515/TJJ.2007.24.1.51

Gorla,, R. and Gorla,, S. () Probabilistic Finite Element Analysis of a Non-Gasketed Flange. International Journal of Turbo and Jet Engines, Vol. 24 (Issue 1), pp. 51-62. https://doi.org/10.1515/TJJ.2007.24.1.51

Gorla,, Rama Subba Reddy and Gorla,, Sreekantha Reddy. "Probabilistic Finite Element Analysis of a Non-Gasketed Flange" International Journal of Turbo and Jet Engines 24, no. 1 (): 51-62. https://doi.org/10.1515/TJJ.2007.24.1.51

Gorla, R, Gorla, S. Probabilistic Finite Element Analysis of a Non-Gasketed Flange. International Journal of Turbo and Jet Engines. ;24(1): 51-62. https://doi.org/10.1515/TJJ.2007.24.1.51

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Articles in the same Issue

CONTENTS
Turbulent Models and Axial Flow Pump Performance Prediction
A Universal Fault Classification for Gas Turbine Diagnosis Under Variable Operating Conditions
Pressure Oscillations in a Single Stage Axial-Flow Low-Speed Compressor during Pre-Stall and Stall
Probabilistic Finite Element Analysis of a Non-Gasketed Flange
Theoretical Formula for Quick Selection of the Number of Blades In Designing Axial-Flow Compressors

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https://doi.org/10.1515/TJJ.2007.24.1.51

Articles in the same Issue

CONTENTS
Turbulent Models and Axial Flow Pump Performance Prediction
A Universal Fault Classification for Gas Turbine Diagnosis Under Variable Operating Conditions
Pressure Oscillations in a Single Stage Axial-Flow Low-Speed Compressor during Pre-Stall and Stall
Probabilistic Finite Element Analysis of a Non-Gasketed Flange
Theoretical Formula for Quick Selection of the Number of Blades In Designing Axial-Flow Compressors