The Effect of Partial Premixing and Heat Loss on the Reacting Flow Field Prediction of a Swirl Stabilized Gas Turbine Model Combustor. [PDF]
Gövert S +4 more
europepmc +1 more source
Discrete imaging models for three-dimensional optoacoustic tomography using radially symmetric expansion functions. [PDF]
Wang K +4 more
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Nonlinear natural engine: Model for thermodynamic processes in mesoscale systems. [PDF]
Wheatley J +4 more
europepmc +1 more source
Perspectives on NO X Emissions and Impacts from Ammonia Combustion Processes. [PDF]
Mashruk S +15 more
europepmc +1 more source
Commentary: an eye on PET quantification. [PDF]
Walker MD, Sossi V.
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Condensed Matter Systems Exposed to Radiation: Multiscale Theory, Simulations, and Experiment. [PDF]
Solov'yov AV +22 more
europepmc +1 more source
Thermoacoustic Instability in Solid Rocket Motor: Non-Normality and Nonlinear Instabilities
An analytical framework is developed to understand and predict the thermoacoustic instability in solid rocket motors, taking into account the non-orthogonality of the eigenmodes of the unsteady coupled system. The coupled system comprises the dynamics of the acoustic field and the propellant burn rate.
Mariappan, Sathesh, Sujith, R. I.
openaire +2 more sources
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