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, und E. Rathakrishnan,

Veröffentlicht/Copyright: 1. März 2006

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Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 23 Heft 1

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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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Published Online: 2006-03

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Artikel in diesem Heft

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

Artikel in diesem Heft

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