Development of a New Tandem Cascade for Axial Flow Fan/Compressor Application

U.K. Saha,; B. Roy,

doi:10.1515/TJJ.1996.13.2.91

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Development of a New Tandem Cascade for Axial Flow Fan/Compressor Application

U.K. Saha, und B. Roy,

Veröffentlicht/Copyright: 1. Juni 1996

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Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 13 Heft 2

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APA
Harvard
Chicago
Vancouver

Saha,, U.K. and Roy,, B.. "Development of a New Tandem Cascade for Axial Flow Fan/Compressor Application" International Journal of Turbo and Jet Engines, vol. 13, no. 2, 1996, pp. 91-102. https://doi.org/10.1515/TJJ.1996.13.2.91

Saha,, U. & Roy,, B. (1996). Development of a New Tandem Cascade for Axial Flow Fan/Compressor Application. International Journal of Turbo and Jet Engines, 13(2), 91-102. https://doi.org/10.1515/TJJ.1996.13.2.91

Saha,, U. and Roy,, B. (1996) Development of a New Tandem Cascade for Axial Flow Fan/Compressor Application. International Journal of Turbo and Jet Engines, Vol. 13 (Issue 2), pp. 91-102. https://doi.org/10.1515/TJJ.1996.13.2.91

Saha,, U.K. and Roy,, B.. "Development of a New Tandem Cascade for Axial Flow Fan/Compressor Application" International Journal of Turbo and Jet Engines 13, no. 2 (1996): 91-102. https://doi.org/10.1515/TJJ.1996.13.2.91

Saha, U, Roy, B. Development of a New Tandem Cascade for Axial Flow Fan/Compressor Application. International Journal of Turbo and Jet Engines. 1996;13(2): 91-102. https://doi.org/10.1515/TJJ.1996.13.2.91

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Published Online: 1996-06

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Artikel in diesem Heft

CONTENTS
Editorial
Interstage Disk-Cavity/Brush Seal Numerical Flow Visualization Study
Development of a New Tandem Cascade for Axial Flow Fan/Compressor Application
Control of the J-85 Turbojet Engine Using the Edmund's Method and the Extended Kaiman Filter Technique
Unsteady Blade Loading and Aeroacoustics of a Pusher Propeller
Study of Hot Streak Phenomena in Subsonic and Transonic Flows
Experimental Investigation of a Small-Aspect-Ratio Elliptic Jet under Pseudolocal Excitation

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https://doi.org/10.1515/TJJ.1996.13.2.91

Artikel in diesem Heft

CONTENTS
Editorial
Interstage Disk-Cavity/Brush Seal Numerical Flow Visualization Study
Development of a New Tandem Cascade for Axial Flow Fan/Compressor Application
Control of the J-85 Turbojet Engine Using the Edmund's Method and the Extended Kaiman Filter Technique
Unsteady Blade Loading and Aeroacoustics of a Pusher Propeller
Study of Hot Streak Phenomena in Subsonic and Transonic Flows
Experimental Investigation of a Small-Aspect-Ratio Elliptic Jet under Pseudolocal Excitation