In this paper, we define a mathematically consistent set of thermo-acoustic equations via asymptotic multiple scale methods in the low-Mach number limit. The final thermoacoustic equations consist of reacting low-Mach number (LMN) equations for hydrodynamic phenomena and acoustic (AC) equations. The two sets of equations are two-way coupled. The coupling terms depend on which multiple scales ar...

A parallel multi-zone method for the simulation of large-scale multidisciplinary applications involving field equations from multiple branches of physics is outlined. The equations of mathematical physics are expressed in a unified form that enables a single algorithm and computational code to describe problems involving diverse, but closely coupled, physics. Specific sub-disciplines include fl...

This study evaluates the performance of a molten carbonate fuel cell and micro gas turbine (MCFC/MGT) hybrid power system bi-fueled by city gas and biogas. The performance of the MCFC/MGT hybrid power system and MFCF/MGT hybrid power system response have been investigated experimentally and numerically. Results show that the MCFC, steam reformer, and catalytic combustor models are in agreement ...

In this study, non-premixed combustion of a traditional fuel-natural gas, and an alternative fuel-biogas, is simulated in swirling flow industrial gas turbine combustor geometry which includes the liner outside casing order to replicate real combustor. The 3D simulations are validated results for both gases analyzed compare evaluate viability biogas as fuel use combustors. performance evaluated...

Particulate matter (soot aerosol or carbon black) emissions from combustion systems have adverse effects on human health and the environment. Soot is a major contributor to the total radiation heat loss in propulsion systems. Soot aerosols in the atmosphere have significant positive radiative forcing that contributes to global warming because of strong absorption of sunlight by soot. As compare...

Combined Cycle Gas Turbine (CCGT) integrates two cyclesBrayton cycle (Gas Turbine) and Rankine cycle (Steam Turbine) with the objective of increasing overall plant efficiency. In modern gas turbine the temperature of the exhaust gases is in the range of 500 oC to 550 oC. Modern steam power plants have steam temperature in the range of 500 oC to 630 oC. Hence gas turbine exhaust can be utilized ...