Modelling of Hypersonic Flow Phenomena

نویسنده

  • J.M.A. Longo
چکیده

Forewords Computational Fluid Dynamic is becoming a mature discipline in aerospace sciences. It is no longer only an analysis tool but ready to be used in all stages of design as well. The materials here presented review the growth and advances done in the last 10 years for hypersonic flow phenomena in continuum regime. The status of the physical modelling, code development issues such as algorithms, surface and field grid generation and validation data is provided. A number of applications examples for ascent vehicles and atmospheric re-entry vehicles are presented based on lessons learned at the German Aerospace Center, DLR, as well as experiences collected from past European technology programs. The materials here presented highlight future areas of research to enhance accuracy, reliability, efficiency, and robustness on modelling hypersonic flow phenomena.

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تاریخ انتشار 2004