We are proud to announce that Ashvin Hosangadi, alongside lead…
Flamelet/Progress Variable Formulation With Pressure Variations for Modeling Rocket Combustion Dynamics Will Be Presented at AIAA SciTech 2024
Conference: AIAA SciTech 2024
Title: Flamelet/Progress Variable Formulation With Pressure Variations for Modeling Rocket Combustion Dynamics
Presenter: Ashvin Hosangadi
Date: Monday, January 8
Session: LP01
Time: 10:50 AM
Abstract: A zonal, multi-physics modeling framework for dynamic combustion processes, that can capture relevant local physics and simulate system behavior while significantly reducing computational cost has been developed. The framework is based on a flamelet/progress variable (FPV) formulation with upgrades to account for dynamic pressure conditions in the combustion chamber. The computational efficiency results from a combination of much smaller number of convective scalar equations and enhanced numerical stability that permits larger time steps than finite-rate kinetics formulation. The FPV framework has been demonstrated on a 3-D configuration featuring a linear array of nine gas-gas, shear coaxial injectors [3][9]. A rigorous evaluation of the ability of the FPV formulation to accurately predict self-excited tangential instabilities has been conducted by comparing both with earlier finite-rate simulations as well as test data [3]. The side wall fluctuations exhibit a 1-T mode, and we obtained a close match for the frequency values as well as the relative amplitudes between the FPV and finite rate formulation (1.3% difference) as well as with the test data (3.7% error). The close match in the frequency and amplitude of the instability predicted by the FPV solution confirms that the FPV formulation provides sufficient accuracy at reduced computational cost.
Presentation Number: AIAA-2024-0152
Authors: Ashvin Hosangadi1, Andrea C Zambon1, Balaji Muralidharan1, Timothy Weathers1, Cheng Huang2, Charles Merkle3
1Combustion Research and Flow Technology Inc, Pipersville, Pennsylvania, United States; 2University of Kansas School of Engineering, Lawrence, Kansas, United States; 3Purdue University System, West Lafayette, Indiana, United States