Numerical Analysis of a Microjet-Based Method for Active Flow Control in Convergent-Divergent Nozzles with a Sudden Expansion Duct

Author:

Aabid Abdul,Afghan Khan Sher,Baig Muneer

Publisher

Computers, Materials and Continua (Tech Science Press)

Subject

General Materials Science

Reference32 articles.

1. A theoretical approximation of the shock standoff distance for supersonic flows around a circular cylinder;Sinclair;Physics of Fluids,2017

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3. Base pressure fluctuations on typical missile configuration in presence of base cavity;Vikramaditya;Journal of Spacecraft and Rockets,2018

4. Response surface analysis of the nozzle flow parameters at supersonic flow through microjets;Al-khalifah;Australian Journal of Mechanical Engineering,2021

5. Numerical analysis of convergent-divergent nozzle using finite element method;Fharukh;International Journal of Mechanical and Production Engineering and Development,2018

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