Laminar Fully Developed Momentum and Heat Transfer of Air With Variable Physical Properties in Isosceles Triangular Ducts

M.B. Ibrahim,; E.H. Buyco,

doi:10.1515/TJJ.1993.10.3.205

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Laminar Fully Developed Momentum and Heat Transfer of Air With Variable Physical Properties in Isosceles Triangular Ducts

M.B. Ibrahim, and E.H. Buyco,

Published/Copyright: September 1, 1993

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From the journal International Journal of Turbo and Jet Engines Volume 10 Issue 3

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MLA
APA
Harvard
Chicago
Vancouver

Ibrahim,, M.B. and Buyco,, E.H.. "Laminar Fully Developed Momentum and Heat Transfer of Air With Variable Physical Properties in Isosceles Triangular Ducts" International Journal of Turbo and Jet Engines, vol. 10, no. 3, pp. 205-224. https://doi.org/10.1515/TJJ.1993.10.3.205

Ibrahim,, M. & Buyco,, E. (). Laminar Fully Developed Momentum and Heat Transfer of Air With Variable Physical Properties in Isosceles Triangular Ducts. International Journal of Turbo and Jet Engines, 10(3), 205-224. https://doi.org/10.1515/TJJ.1993.10.3.205

Ibrahim,, M. and Buyco,, E. () Laminar Fully Developed Momentum and Heat Transfer of Air With Variable Physical Properties in Isosceles Triangular Ducts. International Journal of Turbo and Jet Engines, Vol. 10 (Issue 3), pp. 205-224. https://doi.org/10.1515/TJJ.1993.10.3.205

Ibrahim,, M.B. and Buyco,, E.H.. "Laminar Fully Developed Momentum and Heat Transfer of Air With Variable Physical Properties in Isosceles Triangular Ducts" International Journal of Turbo and Jet Engines 10, no. 3 (): 205-224. https://doi.org/10.1515/TJJ.1993.10.3.205

Ibrahim, M, Buyco, E. Laminar Fully Developed Momentum and Heat Transfer of Air With Variable Physical Properties in Isosceles Triangular Ducts. International Journal of Turbo and Jet Engines. ;10(3): 205-224. https://doi.org/10.1515/TJJ.1993.10.3.205

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Published Online: 1993-09

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CONTENTS
Control of Asymmetrie Systems Using Complex Modes
The Method of Traces of Substantial Surfaces for the Solution of Three-Dimensional Unsteady Flow
Numerical Solution of Three-Dimensional Turbulent Flows for Modern Gas Turbine Components
Laminar Fully Developed Momentum and Heat Transfer of Air With Variable Physical Properties in Isosceles Triangular Ducts
Enhancing Fighter Engine Airstarting Capability
The Stability of Split Flow Fans

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https://doi.org/10.1515/TJJ.1993.10.3.205

Articles in the same Issue

CONTENTS
Control of Asymmetrie Systems Using Complex Modes
The Method of Traces of Substantial Surfaces for the Solution of Three-Dimensional Unsteady Flow
Numerical Solution of Three-Dimensional Turbulent Flows for Modern Gas Turbine Components
Laminar Fully Developed Momentum and Heat Transfer of Air With Variable Physical Properties in Isosceles Triangular Ducts
Enhancing Fighter Engine Airstarting Capability
The Stability of Split Flow Fans