987 resultados para Jet lag


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Denna undersökning har jämfört Finlands och Sveriges cybersäkerhetspolitik. Som forskningsmetod har använts komparativ analys och som teoretisk referensram säkerhetiseringsteorier. Rubriken har valts på grund av den aktuella samhällsdebatt som förs kring cyberssäkerhet. Statliga dokument har använts som primära källor. Intervjuer, artiklar och nyheter har använts för att stöda slutsatserna. Lagstiftningen har lagts i fokus, eftersom den styr själva verkställandet av idkad cybersäkerhetspolitik. Utförd analys visar att Finland och Sverige behandlar cybersäkerhetsfrågorna som en del av den övriga säkerhetspolitiken. Den största skillnaden är att Sverige inte har ett lika synligt behov att säkerhetisera sin cybersäkerhetsagenda. Detta beror på att Sverige redan säkrat sina statliga säkerhetsintressen i cyberrymden tack vare den så kallade FRA-lagen. Analysen visar att Finland med sin säkerhetisering strävar efter likande befogenheter åt myndigheterna att bedriva underrättelse i cyberrymden. Målet för Sveriges säkerhetisering är enligt denna analys att stärka de existerande säkerhetsstrukturerna och utveckla myndighetssamarbete. Lagstiftningsanalysen visar att båda länderna betonar medorgarnas grundläggande friheter och rättigheter, yttrandefrihet samt personlig integritet på nätet. En annan likhet är att båda strävar att lösa lagstiftningsfrågorna genom internationellt samarbete. Den största skillnaden mellan Finland och Sverige är att Sverige endast försöker anpassa den nuvarande lagstiftningen till cyberdomänen, medan Finland strävar att forma en helt ny cyberlagstiftning. Slutsatsen visar dock att staterna först måste definiera cyberterminologin juridiskt, innan de kan göra straffrättsliga tolkningar. Därtill måste länderna utveckla regelverken för överlåtelse av information myndigheterna emellan.

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Jet-cooled, laser-induced phosphorescence excitation spectra (LIP) of thioacetaldehyde CH3CHS, CH3CDS, CD3CHS and CD3CDS have been observed over the region 15800 - 17300 cm"^ in a continuous pyrolysis jet. The vibronic band structure of the singlet-triplet n -* n* transition were attributed to the strong coupling of the methyl torsion and aldehydic hydrogen wagging modes . The vibronic peaks have been assigned in terms of two upper electronic state (T^) vibrations; the methyl torsion mode v^g, and the aldehydic hydrogen wagging mode v^^. The electronic origin O^a^ is unequivocally assigned as follows: CH3CHS (16294.9 cm"'' ), CH3CDS (16360.9 cm"'' ), CD3CHS (16299.7 cm"^ ), and CD3CDS (16367.2 cm"'' ). To obtain structural and dynamical information about the two electronic states, potential surfaces V(e,a) for the 6 (methyl torsion) and a (hydrogen wagging) motions were generated by ab initio quantum mechanical calculations with a 6-3 IG* basis in which the structural parameters were fully relaxed. The kinetic energy coefficients BQ(a,e) , B^(a,G) , and the cross coupling term B^(a,e) , were accurately represented as functions of the two active coordinates, a and 9. The calculations reveal that the molecule adopts an eclipsed conformation for the lower Sq electronic state (a=0°,e=0"') with a barrier height to internal rotation of 541.5 cm"^ which is to be compared to 549.8 cm"^ obtained from the microwave experiment. The conformation of the upper T^ electronic state was found to be staggered (a=24 . 68° ,e=-45. 66° ) . The saddle point in the path traced out by the aldehyde wagging motion was calculated to be 175 cm"^ above the equilibrium configuration. The corresponding maxima in the path taken by methyl torsion was found to be 322 cm'\ The small amplitude normal vibrational modes were also calculated to aid in the assignment of the spectra. Torsional-wagging energy manifolds for the two states were derived from the Hamiltonian H(a,e) which was solved variationally using an extended two dimensional Fourier expansion as a basis set. A torsionalinversion band spectrum was derived from the calculated energy levels and Franck-Condon factors, and was compared with the experimental supersonic-jet spectra. Most of the anomalies which were associated with the interpretation of the observed spectrum could be accounted for by the band profiles derived from ab initio SCF calculations. A model describing the jet spectra was derived by scaling the ab initio potential functions. The global least squares fitting generates a triplet state potential which has a minimum at (a=22.38° ,e=-41.08°) . The flatter potential in the scaled model yielded excellent agreement between the observed and calculated frequency intervals.

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The main objective of the of present study are to study the intraseasonal variability of LLJ and its relation with convective heating of the atmosphere, to establish whether LLJ splits into two branches over the Arabian sea as widely believed, the role of horizonatal wind shear of LLJ in the episodes of intense rainfall events observed over the west coast of India, to perform atmospheric modeling work to test whether small (meso) scale vortices form during intense rainfall events along the west coast; and to study the relation between LLJ and monsoon depression genesis. The results of a study on the evolution of Low Level Jetstream (LLJ) prior to the formation of monsoon depressions are presented. A synoptic model of the temporal evolution of monsoon depression has been produced. There is a systematic temporal evolution of the field of deep convection strength and position of the LLJ axis leading to the genesis of monsoon depression. One of the significant outcomes of the present thesis is that the LLJ plays an important role in the intraseasonal and the interannual variability of Indian monsoon activity. Convection and rainfall are dependent mainly on the cyclonic vorticity in the boundary layer associated with LLJ. Monsoon depression genesis and the episodes of very heavy rainfall along the west coast of India are closely related to the cyclonic shear of the LLJ in the boundary layer and the associated deep convection. Case studies by a mesoscale numerical model (MM5) have shown that the heavy rainfall episodes along the west coast of India are associated with generation of mesoscale cyclonic vortices in the boundary layer.

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Data centre is a centralized repository,either physical or virtual,for the storage,management and dissemination of data and information organized around a particular body and nerve centre of the present IT revolution.Data centre are expected to serve uniinterruptedly round the year enabling them to perform their functions,it consumes enormous energy in the present scenario.Tremendous growth in the demand from IT Industry made it customary to develop newer technologies for the better operation of data centre.Energy conservation activities in data centre mainly concentrate on the air conditioning system since it is the major mechanical sub-system which consumes considerable share of the total power consumption of the data centre.The data centre energy matrix is best represented by power utilization efficiency(PUE),which is defined as the ratio of the total facility power to the IT equipment power.Its value will be greater than one and a large value of PUE indicates that the sub-systems draw more power from the facility and the performance of the data will be poor from the stand point of energy conservation. PUE values of 1.4 to 1.6 are acievable by proper design and management techniques.Optimizing the air conditioning systems brings enormous opportunity in bringing down the PUE value.The air conditioning system can be optimized by two approaches namely,thermal management and air flow management.thermal management systems are now introduced by some companies but they are highly sophisticated and costly and do not catch much attention in the thumb rules.

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This work identifies the importance of plenum pressure on the performance of the data centre. The present methodology followed in the industry considers the pressure drop across the tile as a dependant variable, but it is shown in this work that this is the only one independent variable that is responsible for the entire flow dynamics in the data centre, and any design or assessment procedure must consider the pressure difference across the tile as the primary independent variable. This concept is further explained by the studies on the effect of dampers on the flow characteristics. The dampers have found to introduce an additional pressure drop there by reducing the effective pressure drop across the tile. The effect of damper is to change the flow both in quantitative and qualitative aspects. But the effect of damper on the flow in the quantitative aspect is only considered while using the damper as an aid for capacity control. Results from the present study suggest that the use of dampers must be avoided in data centre and well designed tiles which give required flow rates must be used in the appropriate locations. In the present study the effect of hot air recirculation is studied with suitable assumptions. It identifies that, the pressure drop across the tile is a dominant parameter which governs the recirculation. The rack suction pressure of the hardware along with the pressure drop across the tile determines the point of recirculation in the cold aisle. The positioning of hardware in the racks play an important role in controlling the recirculation point. The present study is thus helpful in the design of data centre air flow, based on the theory of jets. The air flow can be modelled both quantitatively and qualitatively based on the results.

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In the present study the effect of hot air recirculation is studied with suitable assumptions. It identifies that, the pressure drop across the tile is a dominant parameter which governs the recirculation. The rack suction pressure of the hardware along with the pressure drop across the tile determines the point of recirculation in the cold aisle. The positioning of hardware in the racks play an important role in controlling the recirculation point. The present study is thus helpful in the design of data centre air flow, based on the theory of jets. The air flow can be modelled both quantitatively and qualitatively based on the results

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Die fliegerische Tätigkeit auf der Kurzstrecke in der zivilen Luftfahrt unterliegt arbeitsspezifischen Belastungsfaktoren, die sich in wesentlichen Punkten von denen auf der Langstrecke unterscheiden. Eine hohe Arbeitsbelastung auf der Kurzstrecke ist mit vielen Starts und Landungen am Tag verbunden. Neben der Anzahl der Flugabschnitte können auch lange Flugdienstzeiten und/oder unregelmäßige Arbeitszeiten sowie der Zeitdruck während der Einsätze auf der Kurzstrecke zur Belastung für Cockpitbesatzungsmitglieder werden und zu Ermüdungserscheinungen führen. Bisher wurden flugmedizinische und -psychologische Daten hauptsächlich auf der Langstrecke in Bezug auf die Auswirkungen der Jet-Leg Symptomatik und kaum auf der Kurzstrecke erhoben. Deshalb wurde im Rahmen des DLR- Projekts „Untersuchungen zu kumulativen psychischen und physiologischen Effekten des fliegenden Personals auf der Kurzstrecke“ eine Langzeituntersuchung zur Belastung/Beanspruchung, Ermüdung sowie Erholung des Cockpitpersonals auf der Kurzstrecke über jeweils 56 Tage durchgeführt. In Zusammenarbeit mit der Deutschen Lufthansa AG dauerte die Untersuchung zu den Auswirkungen arbeitsspezifischer Belastungsfaktoren auf die Cockpitbesatzungsmitglieder der Boeing 737-Flotte von 2003 bis 2006. ZIEL: Unter Berücksichtigung theoretisch fundierter arbeitspsychologischer Konzepte war das Ziel der Studie, kumulative und akute Effekte auf das Schlaf-Wach-Verhalten, auf die Belastung/Beanspruchung sowie auf die Müdigkeit zu identifizieren, die durch aufeinander folgende Einsätze auf der Kurzstrecke innerhalb eines Zeitraums von acht Wochen auftreten können. Hierfür wurden Daten von 29 Piloten (N=13 Kapitäne; N=16 Erste Offiziere) aufgezeichnet. Das Durchschnittsalter lag bei 33,8 ± 7,9 Jahren (Kapitäne: 42,0 ± 3,8 Jahre; Erste Offiziere: 27,4 ± 2,2 Jahre). METHODEN: Über ein Handheld PC konnten effizient Fragebögen bearbeitet und das Sleep Log sowie das Flight Log geführt werden. Die subjektive Ermüdung und Arbeitsbeanspruchung wurden durch standardisierte Fragebögen (z.B. Ermüdungsskala von Samn & Perelli (1982), NASA-TLX) operationalisiert. Im Sleep Log und im Flight Log wurden das Schlaf-Wach-Verhalten sowie flugspezifische Daten dokumentiert (z.B. Dienstbeginn, Dienstende, Flugabschnitte, Zielorte, etc.). Der Schlaf-Wach-Zyklus wurde mittels der Aktimetrie während des gesamten Messverlaufs aufgezeichnet. Die objektive Leistungsfähigkeit wurde täglich morgens und abends mit Hilfe einer computergestützten Psychomotor Vigilance Task (PVT) nach Dinges & Powell (1985) erfasst. Die Leistung in der PVT diente als Indikator für die Ermüdung eines Piloten. Zusätzliche Befragungen mit Paper-Pencil-Fragebögen sollten Aufschluss über relevante, psychosoziale Randbedingungen geben, die bei den täglichen Erhebungen nicht berücksichtigt wurden (z.B. Arbeitszufriedenheit; Essgewohnheiten; Kollegenbeziehungen). ERGEBNISSE: Unter Beachtung kumulativer Effekte wurde über die Studiendauer keine Veränderung in der Schlafqualität und im Schlafbedürfnis festgestellt. Die Müdigkeit nahm dagegen während der achtwöchigen Untersuchung zu. Die Reaktionszeit in der PVT zeigte an Flugdiensttagen eine Verschlechterung über die Zeit. Insgesamt wurden keine kritischen längerfristigen Effekte analysiert. Akute signifikante Effekte wurden bei der Ermüdung, der Gesamtbelastung und der Leistungsfähigkeit an Flugdiensttagen gefunden. Die Ermüdung als auch die Gesamtbelastung stiegen bei zunehmender Flugdienstdauer und Leganzahl und die Leistung nahm in der PVT ab. Der „time on task“ Effekt zeigte sich besonders in der Ermüdung durch die fliegerische Tätigkeit ab einer Flugdienstzeit von > 10 Stunden und > 4 Legs pro Tag. SCHLUSSFOLGERUNG: Mit diesen Ergebnissen konnte eine wissenschaftliche Datenbasis geschaffen werden aus der Empfehlungen resultieren, wie die Einsatzplanung für das Cockpitpersonal auf der Kurzstrecke unter flugmedizinischen und flugpsychologischen Gesichtspunkten optimiert werden kann. Zudem kann ein sachgerechter Beitrag im Rahmen der Diskussion zur Flugdienst- und Ruhezeitenregelung auf europäischer Ebene geleistet werden.

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We present Very Long Baseline Interferometry (VLBI) observations of the high mass X-ray binary LS I +61˚303, carried out with the European VLBI Network (EVN). Over the 11 hour observing run, performed ~10 days after a radio outburst, the radio source showed a constant flux density, which allowed sensitive imaging of the emission distribution. The structure in the map shows a clear extension to the southeast. Comparing our data with previous VLBI observations we interpret the extension as a collimated radio jet as found in several other X-ray binaries. Assuming that the structure is the result of an expansion that started at the onset of the outburst, we derive an apparent expansion velocity of 0:003 c, which, in the context of Doppler boosting, corresponds to an intrinsic velocity of at least 0:4 c for an ejection close to the line of sight. From the apparent velocity in all available epochs we are able to establish variations in the ejection angle which imply a precessing accretion disk. Finally we point out that LS I +61˚303, like SS 433 and Cygnus X-1, shows evidence for an emission region almost orthogonal to the relativistic jet

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Resumen tomado del propio recurso

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Here we discuss two consecutive MERLIN observations of the X-ray binary LS I +61° 303 . The first observation shows a double-sided jet extending up to about 200 AU on both sides of a central source. The jet shows a bent S-shaped structure similar to the one displayed by the well-known precessing jet of SS 433 . The precession suggested in the first MERLIN image becomes evident in the second one, showing a one-sided bent jet significantly rotated with respect to the jet of the day before. We conclude that the derived precession of the relativistic (beta=0.6) jet explains puzzling previous VLBI results. Moreover, the fact that the precession is fast could be the explanation of the never understood short term (days) variability of the associated gamma-ray source 2CG 135+01 / 3EG J0241+6103