Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts

K. Srinivasan,; S. Elangovan,; E. Rathakrishnan,

doi:10.1515/TJJ.2006.23.1.43

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Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts

K. Srinivasan, , S. Elangovan, and E. Rathakrishnan,

Published/Copyright: March 1, 2006

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From the journal International Journal of Turbo and Jet Engines Volume 23 Issue 1

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Harvard
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Vancouver

Srinivasan,, K., Elangovan,, S. and Rathakrishnan,, E.. "Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts" International Journal of Turbo and Jet Engines, vol. 23, no. 1, 2006, pp. 43-50. https://doi.org/10.1515/TJJ.2006.23.1.43

Srinivasan,, K., Elangovan,, S. & Rathakrishnan,, E. (2006). Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts. International Journal of Turbo and Jet Engines, 23(1), 43-50. https://doi.org/10.1515/TJJ.2006.23.1.43

Srinivasan,, K., Elangovan,, S. and Rathakrishnan,, E. (2006) Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts. International Journal of Turbo and Jet Engines, Vol. 23 (Issue 1), pp. 43-50. https://doi.org/10.1515/TJJ.2006.23.1.43

Srinivasan,, K., Elangovan,, S. and Rathakrishnan,, E.. "Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts" International Journal of Turbo and Jet Engines 23, no. 1 (2006): 43-50. https://doi.org/10.1515/TJJ.2006.23.1.43

Srinivasan, K, Elangovan, S, Rathakrishnan, E. Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts. International Journal of Turbo and Jet Engines. 2006;23(1): 43-50. https://doi.org/10.1515/TJJ.2006.23.1.43

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Articles in the same Issue

CONTENTS
Numerical Investigation of Unsteady Flow in a Low Pressure Turbine
A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers
Numerical Research on the Three Dimensional Unsteady Flow within the Vortex Pump
Variational Principle for 3-D Steady Rotational Flow in Rotor Using Two Stream Functions
Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts
Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor

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https://doi.org/10.1515/TJJ.2006.23.1.43

Articles in the same Issue

CONTENTS
Numerical Investigation of Unsteady Flow in a Low Pressure Turbine
A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers
Numerical Research on the Three Dimensional Unsteady Flow within the Vortex Pump
Variational Principle for 3-D Steady Rotational Flow in Rotor Using Two Stream Functions
Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts
Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor