Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56

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Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56

Airflow from convergent-divergent axisymmetric nozzles expanded into circular duct of higher area were studied experimentally, with the main focus on the flow development in the duct. The flow parameters considered in this investigation are the Mach number at the nozzle exit and the level of expansi...

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Bibliographic Details
Main Authors:	Bashir, Musavir, Baig, Maughal Ahmed Al, Ismail, Ahmad Faris, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	IOSR journals 2016
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL1 Motor vehicles
Online Access:	http://irep.iium.edu.my/54294/ http://irep.iium.edu.my/54294/1/Musavir.pdf

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