An Investigation on Aerodynamic Characteristics of Tab Controlled Axisymmetric and Asymmetric Supersonic Jets

An Investigation on Aerodynamic Characteristics of Tab Controlled Axisymmetric and Asymmetric Supersonic Jets

dc.contributor.guide	Jana, Tamal
dc.coverage.spatial
dc.creator.researcher	Paramesh,Thimmireddigari
dc.date.accessioned	2024-11-22T11:41:54Z
dc.date.available	2024-11-22T11:41:54Z
dc.date.awarded	2024
dc.date.completed	2024
dc.date.registered
dc.description.abstract	Supersonic jet mixing is a critical aspect in the aerospace industry. It plays a pivotal role in mitigating the aeroacoustic noise, improving combustion efficiency and enhancing the stealth characteristics of military aircraft. Therefore the understanding and the precise control of jet mixing is essential. For a comprehensive understanding the present study initially investigates the aerodynamic characteristics of Mach 1.6 axisymmetric supersonic jet. Experimental tests are conducted using an open supersonic jet facility. The quantitative analysis is performed through centerline and radial pressure measurements, while qualitative assessments utilize Schlieren flow visualizations. newline
dc.description.note
dc.format.accompanyingmaterial	None
dc.format.dimensions
dc.format.extent	144p.
dc.identifier.uri	http://hdl.handle.net/10603/602418
dc.language	English
dc.publisher.institution	Aerospace engineering
dc.publisher.place	Bengaluru
dc.publisher.university	Jain University
dc.relation
dc.rights	university
dc.source.university	University
dc.subject.keyword	Engineering
dc.subject.keyword	Engineering Aerospace
dc.subject.keyword	Engineering and Technology
dc.title	An Investigation on Aerodynamic Characteristics of Tab Controlled Axisymmetric and Asymmetric Supersonic Jets
dc.title.alternative
dc.type.degree	Ph.D.