Splitter Plate based Passive and Active Flow Control Study for Tandem Cylinders of Different Geometrical Shapes using a Novel Flexible Forcing Immersed Boundary Scheme based One Step Simplified Lattice Boltzmann Method

dc.contributor.guide	Dash, Sunil Manohar and Sinhamahapatra, Kalyan Prasad
dc.coverage.spatial
dc.creator.researcher	Sikdar, Prabir
dc.date.accessioned	2024-11-18T05:15:58Z
dc.date.available	2024-11-18T05:15:58Z
dc.date.awarded	2024
dc.date.completed	2024
dc.date.registered
dc.description.abstract	newline
dc.description.note
dc.format.accompanyingmaterial	DVD
dc.format.dimensions
dc.format.extent
dc.identifier.uri	http://hdl.handle.net/10603/601307
dc.language	English
dc.publisher.institution	Aerospace Engineering
dc.publisher.place	Kharagpur
dc.publisher.university	Indian Institute of Technology Kharagpur
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	Splitter Plate based Passive and Active Flow Control Study for Tandem Cylinders of Different Geometrical Shapes using a Novel Flexible Forcing Immersed Boundary Scheme based One Step Simplified Lattice Boltzmann Method
dc.title.alternative
dc.type.degree	Ph.D.