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Structural Tailoring/Analysis for Hypersonic Components - A computational simulationThe development of STAHYC (Structural Tailoring/Analysis for Hypersonic Components), a numerical tool for the optimum design of an engine inlet wall panel for hypersonic aerospace vehicles, is described. STAHYC integrates FORTRAN modules of different disciplines, including fluid dynamics, heat transfer, structural analysis, and optimization. The discussion covers the system design concept, system components, system automation, system testing, established links, and data transfer between different computational modules. The various algorithms used in STAHYC are also discussed.
Document ID
19930036327
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Narayanan, G. V. (NASA Lewis Research Center Cleveland, OH, United States)
Reddy, E. S. (NASA Lewis Research Center Cleveland, OH, United States)
Abumeri, G. (Sverdrup Technology, Inc. Brook Park, OH, United States)
Hopkins, Dale A. (NASA Lewis Research Center Cleveland, OH, United States)
Chamis, Christos C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: AIAA(USAF)NASA/OAI Symposium on Multidisciplinary Analysis and Optimization, 4th, Cleveland, OH, Sept. 21-23, 1992, Technical Papers. Pt. 1 (A93-20301 06-66)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 92-4722
Report Number: AIAA PAPER 92-4722
Accession Number
93A20324
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Other

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