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Conjugate Heat Transfer Analysis Capability for Gas Turbine Component Design
- Small Business Information
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Woman-Owned: NoMinority-Owned: NoHUBZone-Owned: No
- Phase 1
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Fiscal Year: 2008Title: Conjugate Heat Transfer Analysis Capability for Gas Turbine Component DesignAgency / Branch: DOD / USAFContract: FA8650-08-M-2842Award Amount: $100,000.00
Abstract:
Turbine performance increases through increasing turbine inlet gas temperature which can result in reduced turbine durability. Currently the design practices employed by the major OEM's for cooled turbine airfoils are generally very empirical in nature and can easily miss important physical behavior thereby compromising airfoil durability. This in turn leads to turbine airfoil durability issues resulting in higher operating costs and weapon system reliability shortcomings. AeroDynamic Solution LLC is propose to develop a robust physics based conjugate heat transfer analysis approach and computational methods that can be readily integrated into the design systems of gas turbine industry OEM's.Small Business Information at Submission:AERODYNAMIC SOLUTIONS LLC
332 Grissom Rd Manchester, CT 06042EIN/Tax ID: 200065836DUNS: N/ANumber of Employees:Woman-Owned: NoMinority-Owned: NoHUBZone-Owned: No
Award Information
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Agency: Department of Defense |
Branch: Air Force |
Award ID: 86621 |
Program Year/Program: 2008 / SBIR |
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Agency Tracking Number: F073-054-1620 |
Solicitation Year: N/A |
Solicitation Topic Code: N/A |
Solicitation Number: N/A |