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Multidisciplinary Analysis of a Hypersonic EngineThe 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.
Document ID
20030068077
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Suresh, Ambady (NASA Glenn Research Center Cleveland, OH, United States)
Stewart, Mark (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2003
Publication Information
Publication: 2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting
Subject Category
Aircraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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