Gust Response Analysis of a Turbine Cascade

Rama Subba Reddy Gorla,; Tondapu Seetharama Reddy,; Dhanireddy Ramalinga Reddy,; Anatole P. Kurkov,

doi:10.1515/TJJ.2003.20.2.115

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Gust Response Analysis of a Turbine Cascade

Rama Subba Reddy Gorla, , Tondapu Seetharama Reddy, , Dhanireddy Ramalinga Reddy, and Anatole P. Kurkov,

Published/Copyright: June 1, 2003

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From the journal International Journal of Turbo and Jet Engines Volume 20 Issue 2

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Gorla,, Rama Subba Reddy, Reddy,, Tondapu Seetharama, Reddy,, Dhanireddy Ramalinga and Kurkov,, Anatole P.. "Gust Response Analysis of a Turbine Cascade" International Journal of Turbo and Jet Engines, vol. 20, no. 2, pp. 115-124. https://doi.org/10.1515/TJJ.2003.20.2.115

Gorla,, R., Reddy,, T., Reddy,, D. & Kurkov,, A. (). Gust Response Analysis of a Turbine Cascade. International Journal of Turbo and Jet Engines, 20(2), 115-124. https://doi.org/10.1515/TJJ.2003.20.2.115

Gorla,, R., Reddy,, T., Reddy,, D. and Kurkov,, A. () Gust Response Analysis of a Turbine Cascade. International Journal of Turbo and Jet Engines, Vol. 20 (Issue 2), pp. 115-124. https://doi.org/10.1515/TJJ.2003.20.2.115

Gorla,, Rama Subba Reddy, Reddy,, Tondapu Seetharama, Reddy,, Dhanireddy Ramalinga and Kurkov,, Anatole P.. "Gust Response Analysis of a Turbine Cascade" International Journal of Turbo and Jet Engines 20, no. 2 (): 115-124. https://doi.org/10.1515/TJJ.2003.20.2.115

Gorla, R, Reddy, T, Reddy, D, Kurkov, A. Gust Response Analysis of a Turbine Cascade. International Journal of Turbo and Jet Engines. ;20(2): 115-124. https://doi.org/10.1515/TJJ.2003.20.2.115

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Published Online: 2003-06

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Articles in the same Issue

CONTENTS
Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft
Gust Response Analysis of a Turbine Cascade
Three Dimensional Navier-Stokes Analysis of a Rigid Wing Configuration
Probabilistic Analysis of Gas Turbine Field Performance
Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section
Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor
Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach
Steady-state Performance Simulation of PT6A-62 Turboprop Engine Using SIMULINK®

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https://doi.org/10.1515/TJJ.2003.20.2.115

Articles in the same Issue

CONTENTS
Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft
Gust Response Analysis of a Turbine Cascade
Three Dimensional Navier-Stokes Analysis of a Rigid Wing Configuration
Probabilistic Analysis of Gas Turbine Field Performance
Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section
Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor
Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach
Steady-state Performance Simulation of PT6A-62 Turboprop Engine Using SIMULINK®