Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine

G.Balu,; S. Panneerselvam,; E. Rathakrishnan,

doi:10.1515/TJJ.2005.22.4.255

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Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine

G.Balu, , S. Panneerselvam, and E. Rathakrishnan,

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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APA
Harvard
Chicago
Vancouver

G.Balu,,, Panneerselvam,, S. and Rathakrishnan,, E.. "Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine" International Journal of Turbo and Jet Engines, vol. 22, no. 4, 2005, pp. 255-264. https://doi.org/10.1515/TJJ.2005.22.4.255

G.Balu,, Panneerselvam,, S. & Rathakrishnan,, E. (2005). Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine. International Journal of Turbo and Jet Engines, 22(4), 255-264. https://doi.org/10.1515/TJJ.2005.22.4.255

G.Balu,., Panneerselvam,, S. and Rathakrishnan,, E. (2005) Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine. International Journal of Turbo and Jet Engines, Vol. 22 (Issue 4), pp. 255-264. https://doi.org/10.1515/TJJ.2005.22.4.255

G.Balu,,, Panneerselvam,, S. and Rathakrishnan,, E.. "Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine" International Journal of Turbo and Jet Engines 22, no. 4 (2005): 255-264. https://doi.org/10.1515/TJJ.2005.22.4.255

G.Balu,, Panneerselvam, S, Rathakrishnan, E. Computational Studies on the Performance of an Isolator for a Dual Mode Scramjet Engine. International Journal of Turbo and Jet Engines. 2005;22(4): 255-264. https://doi.org/10.1515/TJJ.2005.22.4.255

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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.2005.22.4.255

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