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Applications of Response Surface-Based Methods to Noise Analysis in the Conceptual Design of Revolutionary AircraftDue to the growing problem of noise in today's air transportation system, there have arisen needs to incorporate noise considerations in the conceptual design of revolutionary aircraft. Through the use of response surfaces, complex noise models may be converted into polynomial equations for rapid and simplified evaluation. This conversion allows many of the commonly used response surface-based trade space exploration methods to be applied to noise analysis. This methodology is demonstrated using a noise model of a notional 300 passenger Blended-Wing-Body (BWB) transport. Response surfaces are created relating source noise levels of the BWB vehicle to its corresponding FAR-36 certification noise levels and the resulting trade space is explored. Methods demonstrated include: single point analysis, parametric study, an optimization technique for inverse analysis, sensitivity studies, and probabilistic analysis. Extended applications of response surface-based methods in noise analysis are also discussed.
Document ID
20040110957
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hill, Geoffrey A.
(NASA Langley Research Center Hampton, VA, United States)
Olson, Erik D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
June 22, 2004
Subject Category
Acoustics
Report/Patent Number
AIAA Paper 2004-4437
Report Number: AIAA Paper 2004-4437
Meeting Information
Meeting: 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
Location: Albany, NY
Country: United States
Start Date: August 30, 2004
End Date: September 1, 2004
Sponsors: American Inst. of Aeronautics and Astronautics, International Society for Structural and Multidisciplinary Optimization
Funding Number(s)
OTHER: 23-762-45-G2
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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