Conservation of mass relates the mass flow to the induced velocity.
2.
Conservation of energy considers these parameters as well as the induced velocity at the rotor disk.
3.
Blade element theory is combined with momentum theory to alleviate some of the difficulties in calculating the induced velocities at the rotor.
4.
Conservation of linear momentum relates the induced velocity downstream in the far wake field to the rotor thrust per unit of mass flow.
5.
Locating the initial encapsulated electrode closer to the dielectric surface results in induced velocities higher than the baseline case for a given voltage.
6.
Under certain mathematical premises of the fluid, there can be extracted a mathematical connection between power, radius of the rotor, torque and induced velocity.
7.
In the stable configuration, the vorticity, and thus the induced velocity field, will be in a direction that decreases the misalignment and therefore stabilizes the system.
8.
X is the location where induced velocity is produced, x'is the location of the vortex element producing the velocity and c is the chord length of the airfoil.
9.
The definition of F is based on actuator disk models and not directly applicable to BEM . However the most common application multiplies induced velocity term by F in the momentum equations.
10.
Alternatively the variation of the induced velocity along the radius can be modeled by breaking the blade down into small annuli and applying the conservation of mass, momentum and energy to every annulus.
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