Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section

Sanjeev Bharani,; Sidh Nath Singh,; Venkataramaiah Seshadri,; Rajat Kumar Dey,

doi:10.1515/TJJ.2003.20.2.141

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Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section

Sanjeev Bharani, , Sidh Nath Singh, , Venkataramaiah Seshadri, and Rajat Kumar Dey,

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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APA
Harvard
Chicago
Vancouver

Bharani,, Sanjeev, Singh,, Sidh Nath, Seshadri,, Venkataramaiah and Dey,, Rajat Kumar. "Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section" International Journal of Turbo and Jet Engines, vol. 20, no. 2, 2003, pp. 141-154. https://doi.org/10.1515/TJJ.2003.20.2.141

Bharani,, S., Singh,, S., Seshadri,, V. & Dey,, R. (2003). Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section. International Journal of Turbo and Jet Engines, 20(2), 141-154. https://doi.org/10.1515/TJJ.2003.20.2.141

Bharani,, S., Singh,, S., Seshadri,, V. and Dey,, R. (2003) Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section. International Journal of Turbo and Jet Engines, Vol. 20 (Issue 2), pp. 141-154. https://doi.org/10.1515/TJJ.2003.20.2.141

Bharani,, Sanjeev, Singh,, Sidh Nath, Seshadri,, Venkataramaiah and Dey,, Rajat Kumar. "Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section" International Journal of Turbo and Jet Engines 20, no. 2 (2003): 141-154. https://doi.org/10.1515/TJJ.2003.20.2.141

Bharani, S, Singh, S, Seshadri, V, Dey, R. Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section. International Journal of Turbo and Jet Engines. 2003;20(2): 141-154. https://doi.org/10.1515/TJJ.2003.20.2.141

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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.2003.20.2.141

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®