SBIR/STTR Research Award

Dynamic ScreenVanes for the Generation of User-Prescribed, Time-Varying Inlet Distortion

Award identifier 6110f9aeea70f60b637f1328c9800ace527c0f9ca286e49aaabca579ee0a8ed1Awarding agency Department of Defense · Air Force

Award amount

$199,567

Program and phase

STTR · Phase I

Award year

2024

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Technology In Blacksburg Inc
Proposal award date
2024-05-03
Contract end date
2024-10-30
UEI
CLLECDWG5CK6
Solicitation number
23.C
Topic code
AF23C-T003

Research abstract

Next generation air platforms commonly incorporate embedded propulsion systems that can offer both aerodynamics benefits and reduced radar signature. These designs typically require compact offset diffusers that can generate non-uniform flow at the aerodynamic interface plane (AIP). Methods of evaluating the impact of the mean distortion patterns generated by these ducts on engine aeromechanics, performance, and operability have existed for many years. Distortion generating screens have been the industry standard for evaluating total pressure distortion effects in land-based engine tests for decades and more recently StreamVanesTM and ScreenVanesTM, developed by Virginia Tech], have improved the testing capabilities by generating swirl distortion as well as total pressure distortion. Despite these advancements, the need for further improvement remains. Both experiments and scale-resolved simulations of offset diffusers have shown that the resulting exit flow can not only be distorted but also highly unsteady. The impact of this unsteadiness on the engine is currently unknown and further research is necessary. To address this need, the team of Techsburg, Inc. and Virginia Tech are proposing the development of Dynamic ScreenVanes, an advancement on current ScreenVaneTM technology that will be able to produce both mean and time-varying components of fan face distortion. The proposing team will leverage its extensive experience in ScreenVaneTM design, flow control and unsteady aerodynamics to design and evaluate multiple passive and active approaches to adding the unsteady component to their existing distortion generating technology.

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

43 SBIR/STTR records share this UEI (1998–2025). Reported award amounts total $14,258,989. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

Department of Defense

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