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  4. Experimental Studies on Shock-Boundary Layer Controlled Interactions in Supersonic Intake
Please use this identifier to cite or link to this item: http://www.idr.iitkgp.ac.in/xmlui/handle/123456789/11221
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dc.contributor.authorG, Humrutha-
dc.date.accessioned2022-06-15T05:47:51Z-
dc.date.available2022-06-15T05:47:51Z-
dc.date.issued2017-11-
dc.identifier.govdocNB16034-
dc.identifier.urihttp://www.idr.iitkgp.ac.in/xmlui/handle/123456789/11221-
dc.language.isoenen_US
dc.publisherIIT Kharagpuren_US
dc.subjectSonic contraction ratioen_US
dc.subjectIntake capture areaen_US
dc.subjectBoundary layer thicknessen_US
dc.subjectOblique shock angleen_US
dc.subjectHalf angle of the MVGen_US
dc.titleExperimental Studies on Shock-Boundary Layer Controlled Interactions in Supersonic Intakeen_US
dc.typeThesisen_US
Appears in Collections:Experimental Studies on Shock-Boundary Layer Controlled Interactions in Supersonic Intake

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