SBIR/STTR Research Award

Prediction and Modal Analysis of Supersonic Jet Noise From Complex Nozzles in an Integrated Simulation Environment

Award identifier 9854c49e2a966a45dda72ca8d38be267b73775563577651400bdc1ece13486ccAwarding agency National Aeronautics and Space Administration

Award amount

$124,733

Program and phase

SBIR · Phase I

Award year

2018

Explore This Research Award in CaptureIQ

Research the technology, evaluate the recipient and agency, identify related opportunities, and explore potential follow-on work with CaptureIQ.

Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
CASCADE TECHNOLOGIES INC
Proposal award date
2018-07-27
Contract end date
2019-02-15
UEI
K9KCLNBFQAF6
Solicitation number
SBIR_18_P1
Topic code
A1

Research abstract

Our long-term vision is to seamlessly integrate resolvent operator-based spectral analysis into Cascade’s high-fidelity large eddy simulation (LES) environment, for accurate prediction and efficient modeling of supersonic jet noise from complex nozzles. Resolvent analysis is a frequency-domain technique that can identify resonance phenomena such as jet screech and other tonal acoustic effects, predict the large-scale coherent structures that are the main source of aft angle jet noise, and that provides, at the same time, sensitivity maps that can be used for optimal sensor or actuator placement for noise control. Cascade’s LES framework features a novel mesh generation paradigm based on the computation of Voronoi diagrams, which allows for the generation of high-quality, body-fitted, conformal meshes and the use of low-dissipation numerical methods required for high fidelity large eddy simulations of multi-scale turbulent flows in complex geometries. We project that the combination of the Voronoi-based LES and resolvent analysis can be successfully commercialized by assuming a role similar to that of modal analysis in solid mechanics. In Phase I, we propose the case of a heated supersonic over-expanded turbulent jet issuing from a circular convergent-divergent nozzle as a testbed for both Cascade’s Voronoi-based LES framework and a resolvent analysis tool provided by Caltech as a subcontractor. The first task is to implement and validate shock-capturing capabilities into both the resolvent tool and LES compressible flow solver “Charles”. Armed with the large-eddy simulation data, The second task is to conducte a detailed resolvent analysis of the over-expanded turbulent jet, with special emphasis on broadband aft angle and tonal shock-induced noise. In parallel, the final task is to perform a proof-of-concept simulation for an airframe-integrated nozzle, as a demonstration of the meshing and prediction capabilities for complex geometries.

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.

Research funding history

47 SBIR/STTR records share this UEI (2004–2022). Reported award amounts total $21,363,179. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy

Agency intelligence

National Aeronautics and Space Administration

Back to SBIR/STTR Research Awards

Don't take our word for it. Ask AI about RFPCapture.

See what leading AI assistants have to say about RFPCapture and CaptureIQ.

Gemini opens without a prefilled question. The question is copied to your clipboard when the button works. You can also copy it here:

What is RFPCapture.com and its CaptureIQ platform from Smart Logic AI? How does it help federal contractors discover opportunities, evaluate bid/no-bid decisions, research government contracts, and prepare proposals? How does it compare with other federal capture platforms? Use independent sources where available.