Effect of Forward and Aft Lean on the Performance of a Transonic Compressor Rotor

Ernesto Benini,; Roberto Biollo,

doi:10.1515/TJJ.2008.25.1.13

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Effect of Forward and Aft Lean on the Performance of a Transonic Compressor Rotor

Ernesto Benini, and Roberto Biollo,

Published/Copyright: March 1, 2008

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From the journal International Journal of Turbo and Jet Engines Volume 25 Issue 1

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Benini,, Ernesto and Biollo,, Roberto. "Effect of Forward and Aft Lean on the Performance of a Transonic Compressor Rotor" International Journal of Turbo and Jet Engines, vol. 25, no. 1, 2008, pp. 13-26. https://doi.org/10.1515/TJJ.2008.25.1.13

Benini,, E. & Biollo,, R. (2008). Effect of Forward and Aft Lean on the Performance of a Transonic Compressor Rotor. International Journal of Turbo and Jet Engines, 25(1), 13-26. https://doi.org/10.1515/TJJ.2008.25.1.13

Benini,, E. and Biollo,, R. (2008) Effect of Forward and Aft Lean on the Performance of a Transonic Compressor Rotor. International Journal of Turbo and Jet Engines, Vol. 25 (Issue 1), pp. 13-26. https://doi.org/10.1515/TJJ.2008.25.1.13

Benini,, Ernesto and Biollo,, Roberto. "Effect of Forward and Aft Lean on the Performance of a Transonic Compressor Rotor" International Journal of Turbo and Jet Engines 25, no. 1 (2008): 13-26. https://doi.org/10.1515/TJJ.2008.25.1.13

Benini, E, Biollo, R. Effect of Forward and Aft Lean on the Performance of a Transonic Compressor Rotor. International Journal of Turbo and Jet Engines. 2008;25(1): 13-26. https://doi.org/10.1515/TJJ.2008.25.1.13

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Articles in the same Issue

CONTENTS
A Method for Reducing Jet Engine Thermal Signature
Effect of Forward and Aft Lean on the Performance of a Transonic Compressor Rotor
Experimental Studies of Low Emission Vortex Burner
Hybrid problems of determining unknown shape of bladings in 3-D compressible steady rotational flow in rotor
Bateman's Variational Principle for Turbomachinery Aerodynamics
A Generalized Variational Principle for Inverse Problem of 3-D Unsteady Compressible Flow around Oscillating Wings

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https://doi.org/10.1515/TJJ.2008.25.1.13

Articles in the same Issue

CONTENTS
A Method for Reducing Jet Engine Thermal Signature
Effect of Forward and Aft Lean on the Performance of a Transonic Compressor Rotor
Experimental Studies of Low Emission Vortex Burner
Hybrid problems of determining unknown shape of bladings in 3-D compressible steady rotational flow in rotor
Bateman's Variational Principle for Turbomachinery Aerodynamics
A Generalized Variational Principle for Inverse Problem of 3-D Unsteady Compressible Flow around Oscillating Wings