Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor

D. Adler,; Μ. Kleiner,; S. Balaban,

doi:10.1515/TJJ.1996.13.1.25

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Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor

D. Adler, , Μ. Kleiner, and S. Balaban,

Published/Copyright: March 1, 1996

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From the journal International Journal of Turbo and Jet Engines Volume 13 Issue 1

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Adler,, D., Kleiner,, Μ. and Balaban,, S.. "Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor" International Journal of Turbo and Jet Engines, vol. 13, no. 1, pp. 25-34. https://doi.org/10.1515/TJJ.1996.13.1.25

Adler,, D., Kleiner,, Μ. & Balaban,, S. (). Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor. International Journal of Turbo and Jet Engines, 13(1), 25-34. https://doi.org/10.1515/TJJ.1996.13.1.25

Adler,, D., Kleiner,, Μ. and Balaban,, S. () Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor. International Journal of Turbo and Jet Engines, Vol. 13 (Issue 1), pp. 25-34. https://doi.org/10.1515/TJJ.1996.13.1.25

Adler,, D., Kleiner,, Μ. and Balaban,, S.. "Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor" International Journal of Turbo and Jet Engines 13, no. 1 (): 25-34. https://doi.org/10.1515/TJJ.1996.13.1.25

Adler, D, Kleiner, Μ, Balaban, S. Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor. International Journal of Turbo and Jet Engines. ;13(1): 25-34. https://doi.org/10.1515/TJJ.1996.13.1.25

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Published Online: 1996-03

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Articles in the same Issue

CONTENTS
Generalized Euler's Turbomachine Equation and Free Vortex Sheet Conditions in Separated/Cavitated Turbo-Flows
Variable-Domain Finite Element Method Based on Variational Principles for Solving Hybrid Problems of Fully 3-D Compressible Rotor-Flow
Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor
Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method
Active Control of Surge in Multi-Stage Axial-Flow Compressors
Technical Note: Performance of a Miniature Gas Turbine Engine

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https://doi.org/10.1515/TJJ.1996.13.1.25

Articles in the same Issue

CONTENTS
Generalized Euler's Turbomachine Equation and Free Vortex Sheet Conditions in Separated/Cavitated Turbo-Flows
Variable-Domain Finite Element Method Based on Variational Principles for Solving Hybrid Problems of Fully 3-D Compressible Rotor-Flow
Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor
Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method
Active Control of Surge in Multi-Stage Axial-Flow Compressors
Technical Note: Performance of a Miniature Gas Turbine Engine