Surface Heating and Boundary-Layer Transition on a Hypersonic Inflatable Aerodynamic Decelerator
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DOI: 10.2514/1.a34046
Abstract: The aerothermodynamic environment of a hypersonic inflatable aerodynamic decelerator with a flexible thermal protection system has been investigated through wind-tunnel testing. Boundary-layer transition onset locations and surface heating distributions were measured using global phosphor thermography… read more here.
Keywords: hypersonic inflatable; transition; surface; aerodynamic decelerator ... See more keywords