Bateman's Variational Principle for Turbomachinery Aerodynamics

Xin-Wei Zhou,

doi:10.1515/TJJ.2008.25.1.47

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Bateman's Variational Principle for Turbomachinery Aerodynamics

Xin-Wei Zhou,

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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Harvard
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Vancouver

Zhou,, Xin-Wei. "Bateman's Variational Principle for Turbomachinery Aerodynamics" International Journal of Turbo and Jet Engines, vol. 25, no. 1, pp. 47-50. https://doi.org/10.1515/TJJ.2008.25.1.47

Zhou,, X. (). Bateman's Variational Principle for Turbomachinery Aerodynamics. International Journal of Turbo and Jet Engines, 25(1), 47-50. https://doi.org/10.1515/TJJ.2008.25.1.47

Zhou,, X. () Bateman's Variational Principle for Turbomachinery Aerodynamics. International Journal of Turbo and Jet Engines, Vol. 25 (Issue 1), pp. 47-50. https://doi.org/10.1515/TJJ.2008.25.1.47

Zhou,, Xin-Wei. "Bateman's Variational Principle for Turbomachinery Aerodynamics" International Journal of Turbo and Jet Engines 25, no. 1 (): 47-50. https://doi.org/10.1515/TJJ.2008.25.1.47

Zhou, X. Bateman's Variational Principle for Turbomachinery Aerodynamics. International Journal of Turbo and Jet Engines. ;25(1): 47-50. https://doi.org/10.1515/TJJ.2008.25.1.47

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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.2008.25.1.47

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