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High Fidelity Simulation of Jet Noise Emissions from Rectangular Nozzles

Award Information

National Aeronautics and Space Administration
Award ID:
Program Year/Program:
2011 / SBIR
Agency Tracking Number:
Solicitation Year:
Solicitation Topic Code:
Solicitation Number:
Small Business Information
Combustion Research and Flow Technology, Inc.
6210 Kellers Church Road Pipersville, PA -
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Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
Phase 1
Fiscal Year: 2011
Title: High Fidelity Simulation of Jet Noise Emissions from Rectangular Nozzles
Agency: NASA
Contract: NNX11CG70P
Award Amount: $99,979.00


The proposed SBIR Phase I & II programs will lead to the validation of a state-of-the-art Large Eddy Simulation (LES) model, coupled with a Ffowcs-Williams-Hawkings (FW-H) farfield acoustic solver, for supporting the development of advanced engine concepts, including innovative flow control strategies for attenuation of their jet noise emissions. The LES/FW-H model will be simultaneously validated against matched sets of flowfield and companion acoustic data acquired recently at NASA/GRC for round nozzles. The flowfield validation will include detailed comparisons against imagery, mean flow measurements and turbulence statistics. The end-to-end capability of the LES/FW-H noise prediction model will also be demonstrated by applying it to high aspect-ratio rectangular nozzle designs, proposed for testing at NASA GRC under the Fundamental Aeronautics Program. This critical validation will provide the foundation for proceeding to application of this innovative methodology in supporting the design and optimization of control concepts, e.g. chevrons, slot jets, fluidic chevrons, etc., as well as ultimately performing predictions of noise emissions from full-scale, realistic nozzles with complex exhaust flowpaths, airframe/propulsive jet interactions, etc.

Principal Investigator:

Neeraj Sinha
Principal Investigator

Business Contact:

katherine Young
Business Official
Small Business Information at Submission:

Combustion Research and Flow Technology
6210 Keller's Church Road Pipersville, PA 18947-1020

EIN/Tax ID: 232759059
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No