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Articoli di riviste sul tema "Nombre de Stanton"
Verani, Hugo J. "Anthony Stanton, Las primeras voces del poeta Octavio Paz (1931-1938). Ediciones Sin Nombre-CONACULTA, México, 2001; 107 pp." Nueva Revista de Filología Hispánica (NRFH) 52, n. 1 (24 luglio 2017): 227–29. http://dx.doi.org/10.24201/nrfh.v52i1.3249.
Testo completoSchulze, Wolfgang. "Affinal Kin Terms in the East Caucasus". Diachronica 16, n. 1 (6 agosto 1999): 97–122. http://dx.doi.org/10.1075/dia.16.1.06sch.
Testo completoCai, Yue, e Margaret Readdy. "Negative $q$-Stirling numbers". Discrete Mathematics & Theoretical Computer Science DMTCS Proceedings, 27th..., Proceedings (1 gennaio 2015). http://dx.doi.org/10.46298/dmtcs.2503.
Testo completoPechenik, Oliver. "Cyclic Sieving of Increasing Tableaux". Discrete Mathematics & Theoretical Computer Science DMTCS Proceedings vol. AS,..., Proceedings (1 gennaio 2013). http://dx.doi.org/10.46298/dmtcs.12815.
Testo completoTesi sul tema "Nombre de Stanton"
Celep, Muhittin. "Τransitiοn dans les cοuches limites supersοniques : simulatiοns numériques directes et cοntrôle par stries". Electronic Thesis or Diss., Normandie, 2024. http://www.theses.fr/2024NORMIR15.
Testo completoIn high-speed flows, elevated viscous drag and thermal loads are inherent outcomes over aerodynamic bodies. These effects escalate substantially during the transition phase when the boundary layer becomes turbulent. To mitigate potential mechanical damage and fatigue-related failures, thermal protection systems are integrated into vehicles, adding complexity to the technical and economic aspects of design. The solution lies in gaining a comprehensive understanding of transition mechanisms and developing control systems to prolong laminar boundary layer along the vehicle’s surface. Numerous active and passive control techniques can be employed for transition control, with the streak employment method emerging as a particularly promising approach. This method involves generating narrowly spaced streaks in the spanwise direction, creating alternating high and low-speed regions in the flow field. Although the method has only recently been tested in supersonic flows, demonstrating its effectiveness in delaying transition, its suitability needs to be assessed further. In this research work, direct numerical simulations are performed in supersonic and near-hypersonic regimes. Streaks are introduced through a blowing/suction strip placed at the wall prior to that of the perturbation which is used to trigger transition in a “controlled” fashion, forced by a single frequency and wavenumber disturbance. The investigation at Mach 2.0 confirms that streaks with five times the fundamental wavenumber are most beneficial for transition control. Additionally, cooling enhances the method’s effectiveness, while heating severely deteriorates the capability of control streaks. The isothermal wall condition does not alter the comparable stabilizing impact of the mean flow deformation (MFD) and the 3-D part of the control at Mach 2.0. However, at Mach 4.5, both the type of instability and the characteristics of the streaks change significantly. The stabilizing impact of the MFD becomes nearly absent, and the 3-D part of the control predominates, with the characteristics of the streaks no longer considered independent of their initial disturbance amplitude
Simos, Eugenios S. "Géologie et géochimie des indices aurifères de la région de Stanos : Grèce septentrionale". Vandoeuvre-les-Nancy, INPL, 1990. http://www.theses.fr/1990INPL039N.
Testo completoRECCHI, Simonetta. "THE ROLE OF HUMAN DIGNITY AS A VALUE TO PROMOTE ACTIVE AGEING IN THE ENTERPRISES". Doctoral thesis, 2018. http://hdl.handle.net/11393/251122.
Testo completo