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  2. Longitudinal stability - Wikipedia

    en.wikipedia.org/wiki/Longitudinal_stability

    [5] [4] The distance between the center of gravity and the neutral point is defined as "static margin". It is usually given as a percentage of the mean aerodynamic chord . [ 6 ] : 92 If the center of gravity is forward of the neutral point, the static margin is positive.

  3. Center of gravity of an aircraft - Wikipedia

    en.wikipedia.org/wiki/Center_of_gravity_of_an...

    1500 lb * 33.9 in = 50,850 moment (airplane) 100 lb * 68 in = 8,400 moment (baggage) cg = 37 in = (50,850 + 8,400) / 1600 lb (1/2 in out of cg limit) We want to move the CG 1 in using a 100 lb bag in the baggage compartment. shift dist = (total weight * cg change) / weight shifted 16 in = (1600 lb * 1 in) / 100 lb Reworking the problem with 100 ...

  4. Trim drag - Wikipedia

    en.wikipedia.org/wiki/Trim_drag

    Trim drag, denoted as Dm in the diagram, is the component of aerodynamic drag on an aircraft created by the flight control surfaces, [1] mainly elevators and trimable horizontal stabilizers, when they are used to offset changes in pitching moment and centre of gravity during flight.

  5. Centers of gravity in non-uniform fields - Wikipedia

    en.wikipedia.org/wiki/Centers_of_gravity_in_non...

    Textbooks such as The Feynman Lectures on Physics characterize the center of gravity as a point about which there is no torque. In other words, the center of gravity is a point of application for the resultant force. [3] Under this formulation, the center of gravity r cg is defined as a point that satisfies the equation

  6. Pitching moment - Wikipedia

    en.wikipedia.org/wiki/Pitching_moment

    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, / is given by

  7. Center of pressure (fluid mechanics) - Wikipedia

    en.wikipedia.org/wiki/Center_of_pressure_(fluid...

    The center of pressure of an aircraft is the point where all of the aerodynamic pressure field may be represented by a single force vector with no moment. [3] [4] A similar idea is the aerodynamic center which is the point on an airfoil where the pitching moment produced by the aerodynamic forces is constant with angle of attack. [5] [6] [7]

  8. Hermann–Mauguin notation - Wikipedia

    en.wikipedia.org/wiki/Hermann–Mauguin_notation

    However we write ⁠ 4 / m ⁠, not ⁠ 4 / m ⁠, because both 4 and 4 generate four points. In the case of the ⁠ 6 / m ⁠ combination, where 2, 3, 6, 3 , and 6 axes are present, axes 3 , 6 , and 6 all generate 6-point patterns, as we can see on the figure in the right, but the latter should be used because it is a rotation axis – the ...

  9. Improper fraction - Wikipedia

    en.wikipedia.org/?title=Improper_fraction&...

    This page was last edited on 23 June 2020, at 13:36 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may ...