Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Natalia Kuklina"'
Autor:
Doreen Dobritzsch, Judith Meijer, Rutger Meinsma, Dirk Maurer, Ardeshir A. Monavari, Anders Gummesson, Annika Reims, Jorge A. Cayuela, Natalia Kuklina, Jean-François Benoist, Laurence Perrin, Birgit Assmann, Georg F. Hoffmann, Jörgen Bierau, Angela M. Kaindl, André B.P. van Kuilenburg
Publikováno v:
Molecular genetics and metabolism, 136(3), 177-185. Academic Press Inc.
Molecular Genetics and Metabolism, 136(3), 177-185. Academic Press
Molecular Genetics and Metabolism, 136(3), 177-185. Academic Press Inc.
Molecular Genetics and Metabolism, 136(3), 177-185. Academic Press
Molecular Genetics and Metabolism, 136(3), 177-185. Academic Press Inc.
beta-Ureidopropionase is the third enzyme of the pyrimidine degradation pathway and catalyses the conversion of N-carbamyl-beta-alanine and N-carbamyl-beta-aminoisobutyric acid to beta-alanine and beta-aminoisobutyric acid, ammonia and CO2. To date,
Publikováno v:
European Conference on Turbomachinery Fluid Dynamics and hermodynamics.
The present paper continues the investigation started in Part I. The basic turbine stage remains the same as in Part I (an axial turbine stage with axisymmetric nozzles and mean diameter 103.5 mm). The numerical simulation method used in Part I was c
Publikováno v:
European Conference on Turbomachinery Fluid Dynamics and hermodynamics.
The present paper focuses on a comparison of cubic equations of state (EoS) with accurate Span-Wagner (SW) EoS. Aungier Redlich-Kwong (ARK) EoS, Soave Redlich-Kwong (SRK) EoS and standard Peng-Robinson (PR) EoS were chosen as the basic EoS implemente
Publikováno v:
European Conference on Turbomachinery Fluid Dynamics and hermodynamics.
Gas turbine diffusers and exhaust hoods for power generation units are widely studied nowadays. Numerous designs exist as well as empirically derived ratios for optimal performance. Unfortunately, very few of them are appropriate while facing marine
Publikováno v:
European Conference on Turbomachinery Fluid Dynamics and hermodynamics.
The paper focuses on methods for an efficiency increasing of supersonic axial impulse turbines. There was chosen the axial turbine stage with axisymmetric nozzles and mean diameter 103.5 mm as the base model for a numerical and experimental investiga