Numerical Investigation of Single Ramp Scramjet Inlet Characteristics at Mach Number 5.96 Due to Shock Wave–Boundary Layer Interaction
Crossref DOI link: https://doi.org/10.1007/978-981-13-2697-4_20
Published Online: 2018-12-15
Published Print: 2019
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Raja Sekar, K.
Jegadheeswaran, S.
Kannan, R.
Vadivelu, P.
Prasad, G.
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