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Initial Multidisciplinary Design and Analysis FrameworkWithin the Supersonics (SUP) Project of the Fundamental Aeronautics Program (FAP), an initial multidisciplinary design & analysis framework has been developed. A set of low- and intermediate-fidelity discipline design and analysis codes were integrated within a multidisciplinary design and analysis framework and demonstrated on two challenging test cases. The first test case demonstrates an initial capability to design for low boom and performance. The second test case demonstrates rapid assessment of a well-characterized design. The current system has been shown to greatly increase the design and analysis speed and capability, and many future areas for development were identified. This work has established a state-of-the-art capability for immediate use by supersonic concept designers and systems analysts at NASA, while also providing a strong base to build upon for future releases as more multifidelity capabilities are developed and integrated.
Document ID
20100024174
Document Type
Technical Memorandum (TM)
Authors
Ozoroski, L. P. (NASA Langley Research Center Hampton, VA, United States)
Geiselhart, K. A. (NASA Langley Research Center Hampton, VA, United States)
Padula, S. L. (NASA Langley Research Center Hampton, VA, United States)
Li, W. (NASA Langley Research Center Hampton, VA, United States)
Olson, E. D. (NASA Langley Research Center Hampton, VA, United States)
Campbell, R. L. (NASA Langley Research Center Hampton, VA, United States)
Shields, E. W. (ATK-Aerospace Hampton, VA, United States)
Berton, J. J. (NASA Glenn Research Center Cleveland, OH, United States)
Gray, J. S. (NASA Glenn Research Center Cleveland, OH, United States)
Jones, S. M. (NASA Glenn Research Center Cleveland, OH, United States)
Naiman, C. G. (NASA Glenn Research Center Cleveland, OH, United States)
Seidel, J. A. (NASA Glenn Research Center Cleveland, OH, United States)
Moore, K. T. (DB Consulting Group, Inc. Cleveland, OH, United States)
Naylor, B. A. (DB Consulting Group, Inc. Cleveland, OH, United States)
Townsend, S. (ASRC Aerospace Corp. Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
June 1, 2010
Subject Category
Systems Analysis and Operations Research
Report/Patent Number
NASA/TM-2010-216711
L-19768
NF1676L-9500
Funding Number(s)
WBS: WBS 984754.02.07.07.12.04
Distribution Limits
Public
Copyright
Public Use Permitted.

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