A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations

Wu Zhe-min,; Li Hong,; Liu Gao-lian,

doi:10.1515/TJJ.2004.21.1.39

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A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations

Wu Zhe-min, , Li Hong, and Liu Gao-lian,

Published/Copyright: March 1, 2004

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From the journal International Journal of Turbo and Jet Engines Volume 21 Issue 1

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Harvard
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Zhe-min,, Wu, Hong,, Li and Gao-lian,, Liu. "A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations" International Journal of Turbo and Jet Engines, vol. 21, no. 1, 2004, pp. 39-46. https://doi.org/10.1515/TJJ.2004.21.1.39

Zhe-min,, W., Hong,, L. & Gao-lian,, L. (2004). A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations. International Journal of Turbo and Jet Engines, 21(1), 39-46. https://doi.org/10.1515/TJJ.2004.21.1.39

Zhe-min,, W., Hong,, L. and Gao-lian,, L. (2004) A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations. International Journal of Turbo and Jet Engines, Vol. 21 (Issue 1), pp. 39-46. https://doi.org/10.1515/TJJ.2004.21.1.39

Zhe-min,, Wu, Hong,, Li and Gao-lian,, Liu. "A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations" International Journal of Turbo and Jet Engines 21, no. 1 (2004): 39-46. https://doi.org/10.1515/TJJ.2004.21.1.39

Zhe-min, W, Hong, L, Gao-lian, L. A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations. International Journal of Turbo and Jet Engines. 2004;21(1): 39-46. https://doi.org/10.1515/TJJ.2004.21.1.39

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Passive Control of Underexpanded Jets
Statistical Model of Casting Treatment Influence on Compressor Efficiency
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A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow
A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations
Influence of Degradation and Inlet Distortion on Gas Turbine Performance
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https://doi.org/10.1515/TJJ.2004.21.1.39

Articles in the same Issue

CONTENTS
Passive Control of Underexpanded Jets
Statistical Model of Casting Treatment Influence on Compressor Efficiency
Laminar Forced Convection in Curved Channel with Vortex Structures
A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow
A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations
Influence of Degradation and Inlet Distortion on Gas Turbine Performance
Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades