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1causesthe drag force reduction at a lower Reynolds number
but that the above lead to a design conflict at the wing tip where the ideal calls for narrow wing chordsresultingin low Reynolds Numbers and presumably higher drag
that the above lead to a design conflict at the wing tip where the ideal calls for narrow wing chordsresultingin low Reynolds Numbers and presumably higher drag
the above lead to a design conflict at the wing tip where the ideal calls for narrow wing chordsresultingin low Reynolds Numbers and presumably higher drag
the different pressure forcescausinglift , load , thrust , motion , and drag
Horizontal focal plane , rubberized silk double cloth curtain ... speedsettingdial on the top plate , lift and turn
four vector forcesinfluencesthrust , drag , lift and gravity of an aircraft
the protruding piecesmay resultin increased lift and drag force
which factorsinfluencethe lift and drag forces on an aircraft
1:15leadsto a low Reynolds number and laminar flow
Increase in air speedcausesincrease in lift ( and drag
that reduction is n'tcausesthe lift and drag changes
Many researchershave designedairfoils for low Reynolds number
the increase of the rainfall intensitywill resultin the increase of the Reynolds number
which contribute to thrust T and torque Qresultingfrom section lift and drag
to function like an aerofoilresultingin combined forces of lift and drag
the effectscauselift and drag forces to be exerted on
by the wind(passive) caused bythe drag and lift forces
which factorsinfluencethe lift and drag forces
an airfoilresultingforces of lift and drag
built an airplaneto discoverlift , gravity and drag
by air(passive) caused bydrag , lift and momentum
This shape iscontributesto the lift and drag of the airfoil
that the force vector has both a lift and drag componentresultingin lift and drag dipoles
velocities ranging from 4 to 10 m / sresultedin Reynolds numbers ( Re ... up to 346,670
both a lift and drag componentresultingin lift and drag dipoles
the AOA and the inlet speed(passive) are influenced bythe lift and drag coefficient
modethus causingasymmetric lift and drag
according to test specifications(passive) can be independently setThe Reynolds number and Mach number
to 180 and 1.22 x 10 - 4(passive) are setThe Reynolds number and Froude number
the density of the airinfluencesLIFT and DRAG
by body and chassis tested without wings(passive) contributed bylift and drag
by airflow beneath the car(passive) caused bylift and drag
by the movement of wind(passive) caused bythe lift and drag
Both the skin friction ( wall shear ) and pressurecontributeto the drag and the lift
relative wind against the flapswould resultin Lift and drag
can get inside the boatcausingmore lift and drag
the foils will automatically feather themselves into the windthus causingnegligible drag and lift
a surfacecauselift and drag?
The simple mechanism ... any downward slope aft of the front tirewould causelift and drag
the shaft to spin the generator for it to create electricity for home consumptionto causethe shaft to spin the generator for it to create electricity for home consumption
Each related load of the balance system(passive) was setEach related load of the balance system
the shaft to spin the generator for it to produce electricity for home consumptionto causethe shaft to spin the generator for it to produce electricity for home consumption
a > > lift and drag force(passive) caused bya > > lift and drag force
Particles(passive) are influenced byParticles
1 ) Drag(passive) is influenced by1 ) Drag
the aircraft pitching moments(passive) caused bythe aircraft pitching moments
from the disturbed airflowresultingfrom the disturbed airflow
to performance and energy lossesleadingto performance and energy losses
to new tires with better fuel economy and safetycould leadto new tires with better fuel economy and safety
to an increase in the viscosity of the fluidleadsto an increase in the viscosity of the fluid
the aerodynamic performance of airfoil raised ... also the change of Reynolds number and turbulent intensity brought about change in crossing point locationcausedthe aerodynamic performance of airfoil raised ... also the change of Reynolds number and turbulent intensity brought about change in crossing point location
to decrease in the temperature profiles and decrease in Releadsto decrease in the temperature profiles and decrease in Re
the aerodynamic performance of airfoil raisedcausedthe aerodynamic performance of airfoil raised
any vehicle than flightsinfluenceany vehicle than flights
the losses(passive) caused bythe losses
issues with auto - tunepotentially causingissues with auto - tune
the rotor to spin like a propellercausesthe rotor to spin like a propeller
the rotor to spin like a propellercausingthe rotor to spin like a propeller
the rotor to spin like an airplane propellercausesthe rotor to spin like an airplane propeller
the rotor to spin likecausesthe rotor to spin like
to stabilitycontributingto stability
to yawcontributeto yaw
the size and shape of wavescan influencethe size and shape of waves
the rotor to spincausesthe rotor to spin
the rotor to spincausesthe rotor to spin
the effect on the model efficiency(passive) caused bythe effect on the model efficiency
device oscillationcausedevice oscillation
the power coefficient(passive) was influenced bythe power coefficient
a drop in the torque driving force F T , Equation ( 5 ) , and the drag F Dcausesa drop in the torque driving force F T , Equation ( 5 ) , and the drag F D
the rotor to spin , which in turn spins the shaft and the generator in order to produce electricitycausesthe rotor to spin , which in turn spins the shaft and the generator in order to produce electricity
the arm to oscillatecausethe arm to oscillate
for use with individuals with mobility disabilitiesdesignedfor use with individuals with mobility disabilities
the rotor to spin like a propeller and the crankshaft spins a generator to produce electricitycausesthe rotor to spin like a propeller and the crankshaft spins a generator to produce electricity
the power production of a wind turbineinfluencethe power production of a wind turbine
the air foil(passive) caused bythe air foil
in negative aerodynamic damping and lead to gallopingcan resultin negative aerodynamic damping and lead to galloping
the blades to rotatecausesthe blades to rotate
aircraft to flycausesaircraft to fly
from this designresultingfrom this design