SBIR/STTR Research Award

Semi-empirical Bayesian helicopter noise source model

Award identifier b4318ad4f5fa225f40a849bed5ad4c193403637cdd74ef6afd610ec22a87a3cbAwarding agency Department of Defense · Army

Award amount

$196,930

Program and phase

STTR · Phase I

Award year

2024

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Award details

Awarding agency
Department of Defense
Branch
Army
Recipient company
NOISE CONTROL ENGINEERING, LLC
Proposal award date
2023-12-07
Contract end date
2024-05-08
UEI
E2JURKKJTXA1
Solicitation number
23.B
Topic code
A23B-T013

Research abstract

Flight plans are commonly developed for helicopters that perform low-noise operations. There are military cases where these flight plans need to be developed within a matter of hours. These mission planners rely on computer models to accurately and efficiently estimate the noise that will be developed for certain maneuvers. These models depend on accurate estimations of the noise generated by the helicopters æat the sourceÆ. However, developing helicopter noise source models for use in flight path planning is currently limited due to enormous computational time requirements utilizing high fidelity simulations, or by collecting expensive noise measurement data. Development of a physics-based semi-empirical model that can be trained using experimental data will allow mission planners to optimize a large number of flight plans. The proposed approach combines a low-order aerodynamic algorithm with an efficient implementation of the Ffowcs-Williams Hawkings methodology to produce helicopter noise sources for arbitrary flight path conditions. The aerodynamic algorithm implements a modified strip theory/vortex lattice approach to capture the effects of all the relative blade velocity effects and inflow conditions, while a prescribed vortex wake approach will capture any potential blade vortex interactions. The parameters of this model will be set based on historical modelling approaches and can be trained by a Bayesian parameter estimation approach to minimize the noise error between a measured and modeled flight condition. The Bayesian parameter estimation module will couple a parameter subset selection algorithm to identify the minimum number of parameters necessary to efficiently tune the predictive noise estimate. Additionally, a Gaussian process algorithm will tie the model parameters to non-dimensional flight condition hyper-parameters that will model the function that describes how the parameters change with flight conditions. The proposed approach will have the added benefit of quantifying the uncertainty at various stages and allow operators to be confident of the noise sources developed.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

6 SBIR/STTR records share this UEI (1998–2024). Reported award amounts total $2,348,001. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense

Agency intelligence

Department of Defense

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