SBIR/STTR Research Award

Hybrid Prediction Method for Aircraft Interior Noise

Award identifier 04bdddd17d22d570636f3d8d1988365a0ca723f3f52ac171a53a258ec4450ccaAwarding agency National Aeronautics and Space Administration

Award amount

$599,280

Program and phase

SBIR · Phase II

Award year

2006

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ESI US R&D
Proposal award date
2005-12-02
Contract end date
2007-12-03
UEI
Not reported
Solicitation number
Not reported
Topic code
A2.04

Research abstract

The goal of the project is research and development of methods for application of the Hybrid FE-SEA method to aircraft vibro-acoustic problems. This proposal discusses the development and application of new methods of structural-acoustic analysis in order to address existing problems in aircraft interior noise prediction. The proposed methods are based on a hybrid modeling strategy that combines Finite Element Analysis (FEA) and Statistical Energy Analysis (SEA). Over the past five years, Vibro-Acoustic Sciences has devoted a considerable research effort towards the development of a framework for combining these two analysis methods. Recent research carried out by over the past two years has resulted in the development of a rigorous solution to this problem. The resulting Hybrid approach has been derived in general terms and validated for a number of simple structural-acoustic problems. However, the method has not yet been applied to aircraft interior noise prediction. A number of candidate aircraft interior noise problems have been identified which would benefit greatly from the use of the Hybrid method. The aims of the research described in this proposal are therefore: (i) to demonstrate the application of the Hybrid method to a number of existing aircraft interior noise problems, (ii) to develop the method to ensure it contains sufficient functionality to address practical aircraft interior noise problems and (iii) to demonstrate the value of the method in the prediction and reduction of noise in airframe systems.

Technology keywords

Not reported

Awards with the same topic code

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Agency intelligence

National Aeronautics and Space Administration

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