2023
DOI: 10.59287/ijanser.1160
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Design and Computational Analysis of an Axisymmetric Contoured Supersonic Propulsion Nozzle

Abstract: The design of supersonic axisymmetric nozzles to a required exit Mach number necessitates applying the Method of Characteristics (MoC) that reduces the partial differential equations system of hyperbolic form governing such internal flow-fields to two ordinary differential equations known as the characteristic and the compatibility equations. These relationships are then transformed into finite difference equations and solved using an appropriate predictor-corrector algorithm.The present study applies the MoC … Show more

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