it is the difference between local flow direction and free stream direction of atmospheric air
It is a right angle (a 900 angle).
Right angle and rectangle are geometric terms.
An acute angle is one which in geometrical terms measures between 0 and 90 degrees.
Radius Angle Line Plane Hexagon
The common endpoint of an angle is called the vertex. It is the point where the two rays or line segments that form the angle meet. In geometric terms, the vertex is crucial for defining the angle's position and measure.
in simple terms; An attack tends to be an act which is in process. A threat tends to be a promise of an attack to come.
the world comes crumbling down
There is no such thing as an 'induced current'. What is 'induced' is a voltage. If the conductor into which that voltage is induced forms a complete circuit, then a current will result. But it's the voltage that's induced, NOT the current! The direction of the induced voltage is explained by Lenz's Law which, in simple terms, tells us that the direction of the inducted voltage is always such that it will oppose the change in current that causes it. So the induced voltage will oppose any increase in current, but will act in the same direction as a reduction in current.
It is a right angle (a 900 angle).
The formula for the potential energy of a simple harmonic oscillator in terms of the equilibrium position and the angle theta is U 1/2 k (x2 (L - x)2), where U is the potential energy, k is the spring constant, x is the displacement from the equilibrium position, and L is the length of the spring at equilibrium.
Acute angle, algorithm, altitude, angle, area and axis are geometry terms.
terms realated to refraction of light are * interface * incident ray * refracted ray * point of incidence *normal *angle of incidence * angle of refraction *angle of deviation
I can think of only 7 terms. · acute angle · algorithm · altitude · angle · area · arc · axis
offense...
· acute angle
In terms of the Attack and Special Attack stats, Rayquaza is superior.
These are terms that aerospace engineers use to define the flight characteristics that is more associated with the Wing and not the airplane. The shape of a wing will produce different lift and drag for various flight conditions. One parameter is the Angle of Attack. This is the angle that the wing makes with the approaching air flow. A zero(0) Angle of Attack is when the nose of the wing is flying directly into the air flow. As the wing is turns the Nose up, this is a positive angle of attack and this generally results in an increase in Lift. Turning the wing in a nose DOWN is a negative angle of attack and reduces Lift or creates a negative Lift. If the Angle of Attack of the wing gets too large, the wing will stall. Stall occurs with the air flow over the wing is disrupted and does not flow smoothly over the wing. This reduces the Lift drastically. When an airplane pitches its nose up too much, the wing stalls and losses its lift and the airplane will begin to descend. Some airplanes will stall and one wing will drop over and the aircraft will go into a Spin. Modern airplanes, small ones and large passenger airplanes, are designed so that they easily stall into a spin.