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    Multidisciplinary Analysis of a Hypersonic Engine (2003)
    In:  CASI
    Details
    Publication Date: 2018-06-06
    Description: The objective is to develop high fidelity tools that can influence ISTAR design In particular, tools for coupling Fluid-Thermal-Structural simulations RBCC/TBCC designers carefully balance aerodynamic, thermal, weight, & structural considerations; consistent multidisciplinary solutions reveal details (at modest cost) At Scram mode design point, simulations give details of inlet & combustor performance, thermal loads, structural deflections.
    Keywords: Aircraft Propulsion and Power
    Type: 2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting; 129-139; NASA/TM-2003-211896
    Format: application/pdf
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