Preliminary Soot Computations Based on a Model Aircraft Combustor With OpenNCC

Raju, Manthena ; Moder, Jeffrey P ; Wey, Changju T

关键词: SOOT;    AIRCRAFT MODELS;    COMBUSTION;    AIRCRAFT ENGINES;    TURBULENCE MODELS;    COMBUSTION CHAMBERS;    SIMULATION;   

RP-ID  :  ISABE-2019-24007,GRC-E-DAA-TN69431,GRC-E-DAA-TN73425

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

In a preliminary effort to extend our current capabilities used in the design & testing of aero-engine combustors to particulate emissions, we incorporated several existing 2- equation soot models into the Open National Combustion Code (OpenNCC). The paper presents results from a validation study based on a well-characterized, swirl-stabilized, turbulent sooting flame generated by a model aero-engine combustor developed at DLR, Germany. The calculations are based on a Reynolds-Averaged Navier Stokes (RANS) simulation with standard k-e turbulence model & a finite-rate chemical kinetic mechanism. A separate transport equation is solved for all individual species involved in ethylene/air combustion. The predicted velocity and temperature are mostly in good agreement with the measured data and reasonable agreement was found for soot. While the calculated SVF (Soot Volume Fraction) behavior is similar to some other predicted results reported in literature, the measured soot lasts farther downstream than the calculated soot indicating a need for further improvement in the soot models employed.