Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/535054
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dc.coverage.spatial
dc.date.accessioned2023-12-29T12:35:46Z-
dc.date.available2023-12-29T12:35:46Z-
dc.identifier.urihttp://hdl.handle.net/10603/535054-
dc.description.abstractThe objective of the present research is to investigate various design aspects of shaped charge elements and warhead performance at elevated ambient temperatures. There are various elements of a shaped charge warhead like precision initiation coupler, wave shaper etc. The design of these elements has been studied considering their viability for manufacture and performance evaluation methods. newlineShaped charges have been prepared to incorporate metallic liners made of aluminium, soft iron and Oxygen Free Electronic (OFE) copper. These shaped charges were detonated at a fixed stand-off distance from the target. Target damage characteristics have been studied for the three different liner materials. The aluminium liner has induced maximum damage to the target. An additional effect of the blast is available when the aluminium liner is used. This is because less explosive energy is used to deform the aluminium liner and the remaining energy impinges the target in the form of a blast wave that creates additional damage to the target. newline newline
dc.format.extentXXI, 151
dc.languageEnglish
dc.relation
dc.rightsuniversity
dc.titleInvestigation of the Design Aspects and Environmental Conditioning of Shaped Charge Warheads
dc.title.alternative
dc.creator.researcherHarikrishnan, S
dc.subject.keywordEngineering
dc.subject.keywordEngineering Aerospace
dc.subject.keywordEngineering and Technology
dc.description.note
dc.contributor.guideMisra, Ajay and Venkateswara Rao, V
dc.publisher.placePune
dc.publisher.universityDefence Institute of Advanced Technology
dc.publisher.institutionDepartment of Aerospace Engineering
dc.date.registered2016
dc.date.completed2023
dc.date.awarded2023
dc.format.dimensions
dc.format.accompanyingmaterialDVD
dc.source.universityUniversity
dc.type.degreePh.D.
Appears in Departments:Department of Aerospace Engineering

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01_title.pdfAttached File82.05 kBAdobe PDFView/Open
02_prelim pages.pdf809.11 kBAdobe PDFView/Open
03_content.pdf490.89 kBAdobe PDFView/Open
04_abstract.pdf472.75 kBAdobe PDFView/Open
10_annexures.pdf1.35 MBAdobe PDFView/Open
80_recommendation.pdf586.25 kBAdobe PDFView/Open


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