Results 141 to 150 of about 1,003 (200)

The Effect of Partial Premixing and Heat Loss on the Reacting Flow Field Prediction of a Swirl Stabilized Gas Turbine Model Combustor. [PDF]

Flow Turbul Combust, 2018
Gövert S, Mira D, Kok JBW, Vázquez M, Houzeaux G.   +4 more
europepmc   +1 more source

Discrete imaging models for three-dimensional optoacoustic tomography using radially symmetric expansion functions. [PDF]

IEEE Trans Med Imaging, 2014
Wang K, Schoonover RW, Su R, Oraevsky A, Anastasio MA.   +4 more
europepmc   +1 more source

Nonlinear natural engine: Model for thermodynamic processes in mesoscale systems. [PDF]

Proc Natl Acad Sci U S A, 1985
Wheatley J, Buchanan DS, Swift GW, Migliori A, Hofler T.   +4 more
europepmc   +1 more source

Perspectives on NO _X Emissions and Impacts from Ammonia Combustion Processes. [PDF]

Energy Fuels
Mashruk S, Shi H, Mazzotta L, Ustun CE, Aravind B, Meloni R, Alnasif A, Boulet E, Jankowski R, Yu C, Alnajideen M, Paykani A, Maas U, Slefarski R, Borello D, Valera-Medina A.   +15 more
europepmc   +1 more source

Transition to Thermoacoustic Instability in a Turbulent Combustor

Journal of the Combustion Society of Japan, 2018
PAWAR, Samadhan A., SUJITH, Raman I.
openaire   +1 more source

Adaptive control of thermoacoustic combustion instabilities

Adaptive control of thermoacoustic combustion instabilities
identifier:oai:t2r2.star.titech.ac.jp ...
openaire  

Commentary: an eye on PET quantification. [PDF]

Mol Imaging Biol, 2015
Walker MD, Sossi V.
europepmc   +1 more source

Condensed Matter Systems Exposed to Radiation: Multiscale Theory, Simulations, and Experiment. [PDF]

Chem Rev
Solov'yov AV, Verkhovtsev AV, Mason NJ, Amos RA, Bald I, Baldacchino G, Dromey B, Falk M, Fedor J, Gerhards L, Hausmann M, Hildenbrand G, Hrabovský M, Kadlec S, Kočišek J, Lépine F, Ming S, Nisbet A, Ricketts K, Sala L, Schlathölter T, Wheatley AEH, Solov'yov IA.   +22 more
europepmc   +1 more source

Thermoacoustic Instability in Solid Rocket Motor: Non-Normality and Nonlinear Instabilities

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2010
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