NUMERICAL AND EXPERIMENTAL STUDY OF FLUIDIC THRUST VECTORING IN A CONVERGING-DIVERGING NOZZLE USING SHOCK VECTOR CONTROL

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dc.contributor.advisorDarlami, Kamal
dc.contributor.authorShakya, Osika
dc.contributor.authorKunwar, Rashu
dc.contributor.authorShrestha, Shreyas et al
dc.date.accessioned2025-10-15T05:28:44Z
dc.date.available2025-10-15T05:28:44Z
dc.date.issued2025-03
dc.descriptionFluidic thrust vectoring via Shock Vector Control (SVC) offers an efficient alternative to traditional mechanical systems by utilizing secondary flow injection to deflect primary supersonic jet exhaust.
dc.identifier.urihttps://hdl.handle.net/20.500.14540/25278
dc.language.isoen
dc.publisherI.O.E
dc.subjectConverging-Diverging Nozzle
dc.subjectFlow Visualization
dc.subjectFluidic Thrust Vectoring
dc.titleNUMERICAL AND EXPERIMENTAL STUDY OF FLUIDIC THRUST VECTORING IN A CONVERGING-DIVERGING NOZZLE USING SHOCK VECTOR CONTROL
dc.typeProject Report
local.academic.levelOther
local.institute.titleInstitute of Engineering

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