Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice

D.P. Mishra,; D. Mishra,

doi:10.1515/TJJ.2005.22.4.225

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Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice

D.P. Mishra, and D. Mishra,

Published/Copyright: December 1, 2005

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From the journal International Journal of Turbo and Jet Engines Volume 22 Issue 4

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MLA
APA
Harvard
Chicago
Vancouver

Mishra,, D.P. and Mishra,, D.. "Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice" International Journal of Turbo and Jet Engines, vol. 22, no. 4, 2005, pp. 225-236. https://doi.org/10.1515/TJJ.2005.22.4.225

Mishra,, D. & Mishra,, D. (2005). Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice. International Journal of Turbo and Jet Engines, 22(4), 225-236. https://doi.org/10.1515/TJJ.2005.22.4.225

Mishra,, D. and Mishra,, D. (2005) Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice. International Journal of Turbo and Jet Engines, Vol. 22 (Issue 4), pp. 225-236. https://doi.org/10.1515/TJJ.2005.22.4.225

Mishra,, D.P. and Mishra,, D.. "Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice" International Journal of Turbo and Jet Engines 22, no. 4 (2005): 225-236. https://doi.org/10.1515/TJJ.2005.22.4.225

Mishra, D, Mishra, D. Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice. International Journal of Turbo and Jet Engines. 2005;22(4): 225-236. https://doi.org/10.1515/TJJ.2005.22.4.225

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Articles in the same Issue

CONTENTS
Intelligent Control of the F-100 Turbofan Engine for Full Flight Envelope Operation
Numerical Study of Three-Dimensional Jets Using Point Source Method
Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice
Numerical Simulation of Cold Flow in Axisymmetric Dump Combustor
Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine
Performance of Isolator Fed by Laval Nozzle
A New Numerical Approach to Two-Dimensional Stefan Problem
Axial Fan Efficiency: A New Design Approach

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https://doi.org/10.1515/TJJ.2005.22.4.225

Articles in the same Issue

CONTENTS
Intelligent Control of the F-100 Turbofan Engine for Full Flight Envelope Operation
Numerical Study of Three-Dimensional Jets Using Point Source Method
Augmentation of Local and Average Heat Transfer to an Impinging Air Jet Using Orifice
Numerical Simulation of Cold Flow in Axisymmetric Dump Combustor
Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine
Performance of Isolator Fed by Laval Nozzle
A New Numerical Approach to Two-Dimensional Stefan Problem
Axial Fan Efficiency: A New Design Approach