Laminar Forced Convection in Curved Channel with Vortex Structures

A.A. Avramenko,; S.G. Kobzar,; I.V. Shevchuk,; A.V. Kuznetsov,; B.I. Basok,

doi:10.1515/TJJ.2004.21.1.19

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Laminar Forced Convection in Curved Channel with Vortex Structures

A.A. Avramenko, , S.G. Kobzar, , I.V. Shevchuk, , A.V. Kuznetsov, and B.I. Basok,

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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Avramenko,, A.A., Kobzar,, S.G., Shevchuk,, I.V., Kuznetsov,, A.V. and Basok,, B.I.. "Laminar Forced Convection in Curved Channel with Vortex Structures" International Journal of Turbo and Jet Engines, vol. 21, no. 1, 2004, pp. 19-28. https://doi.org/10.1515/TJJ.2004.21.1.19

Avramenko,, A., Kobzar,, S., Shevchuk,, I., Kuznetsov,, A. & Basok,, B. (2004). Laminar Forced Convection in Curved Channel with Vortex Structures. International Journal of Turbo and Jet Engines, 21(1), 19-28. https://doi.org/10.1515/TJJ.2004.21.1.19

Avramenko,, A., Kobzar,, S., Shevchuk,, I., Kuznetsov,, A. and Basok,, B. (2004) Laminar Forced Convection in Curved Channel with Vortex Structures. International Journal of Turbo and Jet Engines, Vol. 21 (Issue 1), pp. 19-28. https://doi.org/10.1515/TJJ.2004.21.1.19

Avramenko,, A.A., Kobzar,, S.G., Shevchuk,, I.V., Kuznetsov,, A.V. and Basok,, B.I.. "Laminar Forced Convection in Curved Channel with Vortex Structures" International Journal of Turbo and Jet Engines 21, no. 1 (2004): 19-28. https://doi.org/10.1515/TJJ.2004.21.1.19

Avramenko, A, Kobzar, S, Shevchuk, I, Kuznetsov, A, Basok, B. Laminar Forced Convection in Curved Channel with Vortex Structures. International Journal of Turbo and Jet Engines. 2004;21(1): 19-28. https://doi.org/10.1515/TJJ.2004.21.1.19

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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

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https://doi.org/10.1515/TJJ.2004.21.1.19

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