
Computational Modeling of Coupled Acoustic and Combustion Phenomena Inherent to Gas Turbine EnginesAward last edited on: 6/23/2023
Sponsored Program
SBIRAwarding Agency
DOD : AFTotal Award Amount
$149,971Award Phase
1Solicitation Topic Code
AF131-181Principal Investigator
Houshang B EbrahimiCompany Information
Phase I
Contract Number: FA9101-13-M-0023Start Date: 5/14/2013 Completed: 2/13/2014
Phase I year
2013Phase I Amount
$149,971Benefit:
Most aerospace technology development programs utilize computational simulation tools, and in particular CFD codes, in conjunction with major experimental/testing efforts. There is a very strong need for high fidelity computational analyses to (1) assist in pre-test planning, (2) design and improve ground test facilities and test techniques, (3) interpret experimental data, (4) provide insight to flow regions where experimental diagnostics are not located, (5) extrapolate results from ground tests to flight conditions, (6) help identify the source of problems, including failures of experiments, and (7) optimize testing to reduce cost and shorten test time. The results of using AUG3D in making such evaluations in the AEDC test work-flow will be carefully documented to help quantify where improvements occur and efficiencies are gained, and to provide guidelines for future users to make the best choices in code settings relative to how the new tool is being used in the test environment.
Phase II
Contract Number: ----------Start Date: 00/00/00 Completed: 00/00/00