at 1×10−6 %(passive) was setThe turbulence intensity
at inlet(passive) was setThe turbulence intensity
to be 10 % for comparison consistency(passive) is setTurbulence intensity
Standard operating room lightscreateturbulence intensity
to be 0.1 %(passive) is setTurbulence intensity
to five percent and an eddy to molecular viscosity ratio of 10(passive) was setTurbulence intensity
to be 3.5 % for primary Boundary conditions of two faces entering a primary nozzle and ejector(passive) was setThe turbulence intensity
at 0.2 % which is slightly above than the experimental reported value of 0.15 % by Karthikeyan et al(passive) is setThe turbulence intensity
Ad run 2 and run 3 ; the validation dataset has been recorded in the easterly flow sector for wind speeds ranging from 6 - 11 m / sresultingin a turbulence intensity
the interactions of radiation with double - diffusive natural convection heat and mass transfer(passive) caused bythe intensity of turbulence
wind shear and buoyancy(passive) is influenced byThe turbulence intensity
Nearby obstructions and structures as well as neighboring turbinescan also influencethe turbulence intensity
transient events at time t(passive) caused byturbulence intensity
equal to abs(val_k(passive) is setThe turbulence intensity
mixed with each otherresultingin high turbulence intensity
the bubble(passive) caused bythe intensity of turbulence
the influence of hilly terrain(passive) caused byturbulence intensity
the jet fluctuations(passive) created byturbulence intensities
u′(passive) was setTurbulence intensity
at a medium intensity(passive) was setThe turbulence intensity
quench zonecauseshigh intensity turbulence
to be 9 %(passive) was setthe turbulence intensity
the environmental parametersinfluencingthe turbulence intensity
the surrounding environment with two different methods(passive) caused bythe turbulence intensity
to 4 % for gas(passive) is setTurbulence intensity
a wake of a wind turbine(passive) caused byIntensity of turbulence
16.0 %(passive) is setThe air turbulence intensity
the trees in the forest(passive) caused byhigh turbulence intensity
the JETFAN objectcan seta turbulence intensity
It is easyto setthe turbulence intensity
climate change(passive) to be influenced byTurbulence intensity
Backflow Turbulent Viscosity RatiosetBackflow Turbulent Viscosity Ratio
to shearing of the liquid phases and the creation of an emulsionwill leadto shearing of the liquid phases and the creation of an emulsion
to 50 % of IEC levelssetto 50 % of IEC levels
Inlet turbulence(passive) was setInlet turbulence
effectively to turbulent flamecontributeseffectively to turbulent flame
in less contrasted turbulent fluxesresultingin less contrasted turbulent fluxes
large , abrupt changes in < AIRCRAFT > altitude and/or attitude ... usually with large variations in indicated airspeed and possibly with momentary loss of controlcauseslarge , abrupt changes in < AIRCRAFT > altitude and/or attitude ... usually with large variations in indicated airspeed and possibly with momentary loss of control
20 % of larvae to settle with KCl induction ( approxcaused20 % of larvae to settle with KCl induction ( approx
from the temporally varying interplay of different rotational flow components ( residual , tidal , near - inertial ) within theBBLresultfrom the temporally varying interplay of different rotational flow components ( residual , tidal , near - inertial ) within theBBL
from the temporally varying interplay of different rotational flow components ( residual , tidal , near - inertial ) within the BBLresultfrom the temporally varying interplay of different rotational flow components ( residual , tidal , near - inertial ) within the BBL
slight , erratic changes in < AIRCRAFT > altitude and/or attitude ( pitch , roll , yaw ) or turbulence that causes slight , rapid and somewhat rhythmic bumpiness without appreciable changes in < AIRCRAFT > altitude or attitude ... lightcausesslight , erratic changes in < AIRCRAFT > altitude and/or attitude ( pitch , roll , yaw ) or turbulence that causes slight , rapid and somewhat rhythmic bumpiness without appreciable changes in < AIRCRAFT > altitude or attitude ... light
the slip velocity of 2–10 mm diameter bubbles , a size commonly encountered in flotation devices(passive) was influenced bythe slip velocity of 2–10 mm diameter bubbles , a size commonly encountered in flotation devices
the magnitude of the varying component ( ie kinetic energysetsthe magnitude of the varying component ( ie kinetic energy
the turbine performances but ... probably most importantmay influencethe turbine performances but ... probably most important
the non - linearities(passive) caused bythe non - linearities
to 5 % , pressure simulation root meanwas setto 5 % , pressure simulation root mean
to higher fatigue loads and an increased failure risk for system componentsleadsto higher fatigue loads and an increased failure risk for system components
the size of particles that are dispersed throughout a fluid , the quality of an emulsion , and the residence time distribution profiles that determine progress and selectivity of chemical reactionsinfluencesthe size of particles that are dispersed throughout a fluid , the quality of an emulsion , and the residence time distribution profiles that determine progress and selectivity of chemical reactions
to the power losses of the next turbineleadto the power losses of the next turbine
a recirculation region enlargementcausinga recirculation region enlargement
from the boundary layer at the top infloworiginatingfrom the boundary layer at the top inflow
in enhanced mixing throughout the intake portresultingin enhanced mixing throughout the intake port
present reduction of 15 - 28 % on the u′ for the actuated casesresultspresent reduction of 15 - 28 % on the u′ for the actuated cases
to five percent ( 5 % ) to emulate the production of turbulence for both RG1 and RG2 casesis setto five percent ( 5 % ) to emulate the production of turbulence for both RG1 and RG2 cases
to localized scourcan leadto localized scour
the requirements(passive) set bythe requirements
to the kappa - like steady - state particle distribution ( 42 ) , $ $ I_L(k)=\frac{\kappa'}{\kappa}\frac{T_e}{4\pi^2 } \biggl(1 + \frac{\omega_{pe}^2}{\kappa'\,k^2v_{Te}^2 } \biggr),$$ where \(v_{Te}^{2}=2T_{e}/m_{e}\leadsto the kappa - like steady - state particle distribution ( 42 ) , $ $ I_L(k)=\frac{\kappa'}{\kappa}\frac{T_e}{4\pi^2 } \biggl(1 + \frac{\omega_{pe}^2}{\kappa'\,k^2v_{Te}^2 } \biggr),$$ where \(v_{Te}^{2}=2T_{e}/m_{e}\
during the experimentcreatedduring the experiment
at its default 2 %settingat its default 2 %
hard galloping to become soft and soft galloping to become weaker before eventually disappearingcauseshard galloping to become soft and soft galloping to become weaker before eventually disappearing
the skin friction increase(passive) caused bythe skin friction increase
the performance of NAIcan influencethe performance of NAI
present reduction of 20 % on the u′ for the actuated casesresultspresent reduction of 20 % on the u′ for the actuated cases
from boundary layer tripping / separation Provides aircrew , UAS operators and avionics systems with vital information that is currently not available to themresultingfrom boundary layer tripping / separation Provides aircrew , UAS operators and avionics systems with vital information that is currently not available to them
the value of the turbulence intensity for the LES modelsetsthe value of the turbulence intensity for the LES model