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pro vyhledávání: '"Saifuddin, K. S."'
Autor:
Nagashetty, K., Saifuddin, K. S., Saravanan, S., Gurumurthy, K. S., Jagadeesh Gopalan, Reddy, K. P. J.
Publikováno v:
Scopus-Elsevier
The flowfield around large angle blunt cones flying at hypersonic Mach numbers is complex with a strong detached shock wave in front. Visualization of these shock waves around the test models in groundbased testing facilities is an essential part of