Supersonic Combustion Flow Visualization at Hypersonic Flow
نویسنده
چکیده
Currently, a new generation of scientific aerospace vehicles, using advanced hypersonic airbreathing propulsion based on supersonic combustion technology, is in development at several research centers [1]. The 14-X Brazilian Hypersonic Aerospace Vehicle, Figure 1, designed by Rolim et al. [2], at the Prof. Henry T. Nagamatsu Laboratory of Aerothermodynamics and Hypersonics, Figure 2, at the Institute for Advanced Studies (IEAv), is part of the continuing effort of the Department of Aerospace Science and Technology (DCTA), to develop a technological demonstrator using: i) ”waverider” technology to provide lift to the aerospace vehicle, and ii) ”scramjet” technology to provide hypersonic airbreathing propulsion system based on supersonic combustion.
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