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Aircraft Conceptual Structural Design Using the AMMIT Structural Analysis ToolAircraft conceptual structural design is the process of developing and refining an idea for an aircraft into a feasible structural design. The process typically involves multiple evaluations of a single configuration and can require designers to examine thousands of concepts. Standard approaches to conducting structural analyses in this phase are either based on the use of historical or empirical data or often require significant expertise in structural analysis to perform these rapid assessments. The AMMIT structural analysis tool includes structural line models and handbook methods wrapped in a simple to use interface that can enable rapid, physics-based structural designs without requiring extensive structural expertise. The objectives of the present paper are to introduce AMMIT, describe the methods used in AMMIT, and present the results of the validation effort. Validation of the AMMIT methodology was performed on nine aircraft to determine the accuracy of the methods, highlight features of AMMIT, and guide future development of the methodology. Results of the validation effort indicated that AMMIT provides a prediction of primary structural weight for each aircraft with an acceptable level of error during the preliminary design phase with a minimal expenditure of computational resources.


Document ID
20200002410
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Horvath, Bryce L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 14, 2020
Publication Date
January 7, 2019
Subject Category
Structural Mechanics
Systems Analysis And Operations Research
Report/Patent Number
NF1676L-30317
Report Number: NF1676L-30317
Meeting Information
Meeting: 2019 AIAA SciTech Forum and Exposition
Location: San Diego, CA
Country: United States
Start Date: January 7, 2019
End Date: January 11, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 109492.02.07.01.10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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