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Handbook of Research on Aspects and Applications of Incompressible and Compressible Aerodynamics

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dc.creator Angelin S., Irish
dc.creator Gürbüz, Habib
dc.creator Shankar R., Naren
dc.date 2022-07-01T00:00:00Z
dc.date.accessioned 2023-01-09T12:02:16Z
dc.date.available 2023-01-09T12:02:16Z
dc.identifier 47d3a89f-a4be-4d30-9d0b-03bf25570a24
dc.identifier https://avesis.sdu.edu.tr/publication/details/47d3a89f-a4be-4d30-9d0b-03bf25570a24/oai
dc.identifier.uri http://acikerisim.sdu.edu.tr/xmlui/handle/123456789/97809
dc.description <p><span style="color: rgb(51, 51, 51); font-family: Arial, Verdana, Helvetica, sans-serif; font-size: 12px;">Hypersonic vehicles attain a speed five times more high-speed than the speed of sound, which is beyond Mach 5 and nearly equal to 6174km/h. Hypersonic flow has certain characteristics, essentially a reedy shock layer, formation of entropy layer, viscous interactions, high temperature, and low-density flow. Only if these characteristics are subjected in the flow can the flow can be called hypersonic. While designing a hypersonic flight vehicle, the characteristics of the hypersonic atmosphere should be understood clearly. This comes as a major design constraint. A brief overview of the hypersonic vehicle design and high-speed flow characteristics will be presented in this chapter. A few characteristics of hypersonic flow and the ideal design conditions will also be reviewed.</span><br></p>
dc.language eng
dc.rights info:eu-repo/semantics/closedAccess
dc.title Handbook of Research on Aspects and Applications of Incompressible and Compressible Aerodynamics
dc.type info:eu-repo/semantics/bookPart


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