SBIR/STTR Research Award

Multiphysics, Coupled Analysis Framework for Hypersonic Vehicle Structures

Award identifier e87695c4256c27cc8e3f8eab60030c570318bd3617c0c673968361c7b68c8365Awarding agency Department of Defense · Air Force

Award amount

$99,350

Program and phase

SBIR · Phase I

Award year

2009

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
ATA ENGINEERING, INC.
Proposal award date
2008-12-22
Contract end date
2009-11-19
UEI
PNZEUK9JC187
Solicitation number
2008.3
Topic code
AF083-181

Research abstract

This proposal addresses the development of a practical multiphysics coupled analysis framework for hypersonic vehicle structures. This Phase I SBIR has two parts. The first part involves the definition of a hypersonic vehicle mission and its aero-thermal environments to locate and characterize regions where tightly coupled analysis will be necessary. This will include a thorough review of the current state-of-the-art analysis methods and identification of the current limitations of each method in the context of the desired prediction confidence levels. The second part involves the development of a conceptual framework, using appropriate state-of-the-art multiphysics tools, to simulate the response of high-speed vehicle structures in those environments. As the proposed program requires integration of multiple engineering disciplines in order to achieve a best, practical solution, the SBIR team will utilize various areas of expertise within ATA Engineering, along with expert subcontractors. ATA and its partner at Mississippi State University have already successfully developed related multiphysics components, including coupled thermo-structural analysis, coupled aeroelastic analysis, and coupled aero-vibro-acoustic analysis. BENEFIT: The improved predictive accuracy of the multiphysics coupled analysis tool that will be developed under this SBIR will be a key enabler in the future development of hypersonic air vehicles that must withstand extreme aero-thermal and aero-acoustic environments. Applications in the DoD market include reusable and single-use military hypersonic vehicles, as well as stealth aircraft with ducted exhaust. In other commercial markets, a coupled fluid-thermal-structural design tool would have application to nuclear engineering and related DoE applications. An unsteady CFD tool that could accurately predict fluctuating pressure levels (FPL) loading under turbulent boundary layers and aerodynamic shocks would have very wide application.

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

125 SBIR/STTR records share this UEI (2002–2025). Reported award amounts total $58,455,367. 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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