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Investigation of Hypersonic Conic Flows Generated by Magnetoplasma Light-Gas Gun Equipped With Laval Nozzle
[chapter]
2021
Hypersonic Vehicles - Applications, Recent Advances, and Perspectives [Working Title]
Preserved Fulltext
This chapter introduces new approach of hypersonic flow generation and experimental study of hypersonic flows over cones with half- angles τ1 = 3◦ and τ2 = 12◦. Mach number of the of the incident flow was M1 = 18. Visualization of the flow structure was made by the schlieren method. Straight Foucault knife was located in the focal plane of the receiving part of a shadow device. Registration of shadow patterns was carried out using high- speed camera Photron Fastcam (300 000 fps) with an
doi:10.5772/intechopen.99457
fatcat:lskissqwgrfofewgjtil24rx5y