Characterization Of Shock Tunnel With Shock Angle

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dc.contributor.advisorBhattarai, Sudip
dc.contributor.authorAdhikari, Chandrika Nand
dc.date.accessioned2025-05-04T04:58:56Z
dc.date.available2025-05-04T04:58:56Z
dc.date.issued2025-04-08
dc.descriptionA shock tube is a standard laboratory apparatus to study shock waves since it can produce different regimes and flow rates. The abrupt release of energy, high-speed projectiles, laser ablations, and supersonic or transonic objects moving (typically with a Mach number of 0.3) all produce such waves.
dc.identifier.urihttps://hdl.handle.net/20.500.14540/24973
dc.language.isoen
dc.publisherPulchowk Campus
dc.titleCharacterization Of Shock Tunnel With Shock Angle
dc.typeThesis
local.academic.levelMasters
local.affiliatedinstitute.titlePulchowk Campus
local.institute.titleInstitute of Engineering

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