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pitching moment : ウィキペディア英語版
pitching moment

In aerodynamics, the pitching moment on an airfoil is the moment (or torque) produced by the aerodynamic force on the airfoil if that aerodynamic force is considered to be applied, not at the center of pressure, but at the aerodynamic center of the airfoil. The pitching moment on the wing of an airplane is part of the total moment that must be balanced using the lift on the horizontal stabilizer.〔Clancy, L.J., ''Aerodynamics'', Section 5.3〕 More generally, a pitching moment is any moment acting on the pitch axis of a moving body.
The lift on an airfoil is a distributed force that can be said to act at a point called the center of pressure. However, as angle of attack changes on a cambered airfoil, there is movement of the center of pressure forward and aft. This makes analysis difficult when attempting to use the concept of the center of pressure. One of the remarkable properties of a cambered airfoil is that, even though the center of pressure moves forward and aft, if the lift is imagined to act at a point called the aerodynamic center the moment of the lift force changes in proportion to the square of the airspeed. If the moment is divided by the dynamic pressure, the area and chord of the airfoil, to compute a pitching moment coefficient, this coefficient changes only a little over the operating range of angle of attack of the airfoil. The combination of the two concepts of ''aerodynamic center'' and ''pitching moment coefficient'' make it relatively simple to analyse some of the flight characteristics of an aircraft.〔Clancy, L.J., ''Aerodynamics'', Section 5.10〕
==Measurement==
The aerodynamic center of an airfoil is usually close to 25% of the chord behind the leading edge of the airfoil. When making tests on a model airfoil, such as in a wind-tunnel, if the force sensor is not aligned with the quarter-chord of the airfoil, but offset by a distance x, the pitching moment about the quarter-chord point, M_ is given by
:M_ = M_\text + \mathbf\times (D_\text, L_\text)
where the indicated values of ''D'' and ''L'' are the drag and lift on the model, as measured by the force sensor.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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