NASA NTRS · 20030068077
Multidisciplinary Analysis of a Hypersonic Engine
Abstract
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.
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Suresh, Ambady, Stewart, Mark. 2003-08-01. Multidisciplinary Analysis of a Hypersonic Engine. https://ntrs.nasa.gov/citations/20030068077
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