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flexion decreases in angle between articulating bones extension increases in angle between articulation bones
It does. But when the ray arrives perpendicular to the boundary, the angle of incidence and the angle of refraction are both zero, so its direction doesn't change.
As the angle of incidence is increased, angle of deviation 'd' decreases and reaches minimum value. If the angle of incidence is further increased, the angle of deviation is increased. Let dm be the angle of minimum deviation. The refracted ray in the prism in that case will be parallel to the base.
The wing twist angle is introduced to prevent stall from occurring at the wing tip before than the wing root. Usually wings are 'washout' twisted, resulting in a decreasing angle of attack starting from the root and towards the tip. Precisely, the twist angle is the angle between the zero-lift line of the profile in the current section and the zero-lift line of the root profile. As the twist angle increases along the span, the lower is the local angle of attack and the lower is the lift generated. By this we prevent the wing tip from generating as much lift as the wing root, which may cause the stall to occur at the worst place we'd like it to occur, the ailerons. By washout twist, we obtain to make stall occur at the wing root, without lost of ailerons control.
-- Light approaches the boundary between any two media along the normal direction. -- Light approaches the boundary at any angle and the indexes of refraction of both media are equal.
As trust increases, speed increases. Providing the angle of attack, and the wind speed stay the same.
The angle of reflection increases also.
Increases
No. As the angle increases from zero to 90 degrees,its sine increases from zero to '1'.
The number of images increases
The angle if refraction also increases.
It varies for all blades collectively as you pull up or push down on the collective. and alternates from side-to-side and front-to back as you move the cyclic. If you move the cyclicto the right it decreases the angle of attack on the right side and increases the angle of attack on the left side. Since the right side loses lift and the left side gains lift the helicopter will bank and turn to the right.The angle of attack of all the blades at hover will be about zero.
The energy efficiency increases as the angle increases.
The angle of attack is the angle that the kite flys into the air at. The angle depends on the wind seeded in the area you are flying the kite in.
It gets refracted so that its direction of propagation is the boundary line.
Stephen P. Wilkinson has written: 'A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel' -- subject(s): Pressure gradients, Cooling, Boundary layer stability, Hypersonic boundary layer, Additives, Angle of attack
no