SBIR/STTR Research Award

Hypersonic Propulsion: Improvements in Controls and Instrumentation

Award identifier 5a45ca4d946da512a6f160d6a9d195ea3802f7b16b24db69ad0627aca49921d4Awarding agency Department of Defense · Air Force

Award amount

$149,926

Program and phase

SBIR · Phase I

Award year

2012

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
INNOVATIVE SCIENTIFIC SOLUTIONS INC
Proposal award date
2011-11-02
Contract end date
Not reported
UEI
GE6SB9D2NFM3
Solicitation number
2011.2
Topic code
AF112-182

Research abstract

ABSTRACT: Among the technical challenges associated with current Air Force scramjet technology development is coupling between the combustor and isolator that leads to isolator unstart. Performance is currently restricted because the engine is not actively controlled. While simple passive techniques such as cavities for shock capture exist, they result in increased drag. We propose a closed-loop control scheme that seeks to actively isolate the inlet from the combustor to prevent unstart while monitoring and minimizing the drag in the inlet using flow control. The shock trapping scheme is based on a cavity in the isolator section and the flow control system consists of arc filament plasma actuators coupled with skin friction sensors. When there is potential for unstart, the actuators will make the cavity a high drag cavity, which would act as a shock trapping device. In normal operation, the actuators will be adjusted to minimize the drag of the cavity. The skin friction sensors that are based on an existing Surface Stress Sensitive Film sensor hardened to operate in high enthalpy flows. The flow control scheme is based on a class of high amplitude and high bandwidth plasma actuators called localized arc filament plasma actuators. BENEFIT: Surface Stress Sensitive Films are being investigation for a variety of applications in aerodynamics, hydrodynamics, and biomedical research. Skin friction is a quantity of interest in many aerodynamics applications such as validation of CFD, and investigation of hypersonic inlets. A point version of this sensor could be used for both ground test and flight test measurements of skin friction. Other applications include a sensor for feedback in closed loop flow control. The S3F sensor has recently been used to detect shear forces on tires and a means of using the system for predictive maintenance of fleet vehicles is underway. The sensor also has use in biomedical applications include ongoing research for identification and correlation of shear on the foot of diabetics. The formation of bed sores is believed to be related to shear stress, and therefore this would be a similar application of the technology. Other biomedical applications include shear stress on surfaces of artificial implants such as stints, hearts, valves, and assist pumps

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

142 SBIR/STTR records share this UEI (1996–2024). Reported award amounts total $54,859,887. 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, Department of Agriculture, Department of Health and Human Services, National Science Foundation, Department of Energy

Agency intelligence

Department of Defense

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