1/14/2024 0 Comments Apollo 4 combustion instability![]() Gurrala SR, Shaija A Computational analysis of reacting flows in afterburner. In: 19th annual conference on liquid atomization and spray systems, Toronto Canada, (2006)ĪNSYS, Inc., “ANSYS Fluent Theory Guide,” Canonsburg, PA, U.S.A., Release 15.0, ANSYS, Inc., November 2013.įree Field Technologies. ![]() Ind J Eng Mater Sci 11:31–37Įbrahimi JB (2006) Overview of gas turbine augmentor design, operation and combustion oscillation, ILASS Americas. Unaune SV, Ganesan V (2005) Analysis of reacting flows in an aero-engine afterburner using computational fluid dynamics. Useller JW, Braithwaite WM, Rudy CJ (1954) Influence of combustion chamber length on afterburner performance. Because of the many development programs during the Apollo period, most of the combustion stability research data and analytical tools are of the 1950's and 1960s. These acoustic vibrations cause fatigue failure of the combustor and decrease the combustion efficiency. ![]() thesis, Department of Aerospace Engineering, Indian Institute of Science, Bangalore The thermo-acoustic instability in the combustion process of a gas turbine is caused by the interaction of the heat release mechanism and the pressure perturbation. Kampa A (2007) Combustion instability screech in gas turbine afterburners. ![]()
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