Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance

M. Govardhan,; B.H.L. Gowda,; G. Kishor,

doi:10.1515/TJJ.2000.17.4.303

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Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance

M. Govardhan, , B.H.L. Gowda, and G. Kishor,

Published/Copyright: December 1, 2000

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From the journal International Journal of Turbo and Jet Engines Volume 17 Issue 4

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APA
Harvard
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Vancouver

Govardhan,, M., Gowda,, B.H.L. and Kishor,, G.. "Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance" International Journal of Turbo and Jet Engines, vol. 17, no. 4, pp. 303-318. https://doi.org/10.1515/TJJ.2000.17.4.303

Govardhan,, M., Gowda,, B. & Kishor,, G. (). Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance. International Journal of Turbo and Jet Engines, 17(4), 303-318. https://doi.org/10.1515/TJJ.2000.17.4.303

Govardhan,, M., Gowda,, B. and Kishor,, G. () Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance. International Journal of Turbo and Jet Engines, Vol. 17 (Issue 4), pp. 303-318. https://doi.org/10.1515/TJJ.2000.17.4.303

Govardhan,, M., Gowda,, B.H.L. and Kishor,, G.. "Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance" International Journal of Turbo and Jet Engines 17, no. 4 (): 303-318. https://doi.org/10.1515/TJJ.2000.17.4.303

Govardhan, M, Gowda, B, Kishor, G. Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance. International Journal of Turbo and Jet Engines. ;17(4): 303-318. https://doi.org/10.1515/TJJ.2000.17.4.303

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Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows
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Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance
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https://doi.org/10.1515/TJJ.2000.17.4.303

Articles in the same Issue

CONTENTS
Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows
Characteristics of Arrays of Spray Diffusion Flames
Maximizing Multistage Turbine Efficiency by Optimizing Hub and Shroud Shapes and Inlet and Exit Conditions of Each Blade Row
Experimental Evaluation of Precursors to Centrifugal Compressor Instability
3-D Inlet Guide Vane Generated Vortical Forcing Functions
Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance
A New Era of Jet Transport Safety By Advanced Legislation?