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- Static_margin abstract "If an aircraft in flight suffers a disturbance in pitch that causes an increase (or decrease) in angle of attack, it is desirable that the aerodynamic forces on the aircraft cause a decrease (or increase) in angle of attack so that the disturbance does not cause a continuous increase (or decrease) in angle of attack. This is longitudinal static stability.Static margin is a concept used to characterize the static longitudinal stability and controllability of aircraft and missiles.In aircraft analysis, static margin is defined as the distance between the center of gravity and the neutral point of the aircraft, expressed as a percentage of the mean aerodynamic chord of the wing. The greater this distance and the narrower the wing, the more stable the aircraft. Conventionally, the neutral point is aft of the c.g., although in rare cases (computer controlled fighter aircraft) it may be forward of the c.g., i.e. slightly unstable, to obtain quickness of response in combat. Too great longitudinal stability makes the aircraft \"stiff\" in pitch, resulting in such undesirable features as difficulty in obtaining the necessary stalled nose-up pitch when landing.The position of the neutral point is found by taking the algebraic net moment of all horizontal surfaces, measured from the nose of the aircraft, in the same manner as the c.g. is determined, i.e. the sum of all such moments divided by their total area. The stabilizer and elevator dominate this result, but it is necessary to account for all surfaces such as fuselage, landing gear, prop-normal, etc. It is also necessary to take account of the center of pressure of the wing, which can move a good deal fore and aft as angle of attack of a flat-bottom wing section (Clark Y) changes, or not at all in the case of self-stabilizing sections such as the M6.The neutral point in conventional aircraft is a short distance behind the c.g. (\"The feathers of the arrow must be at the back\"); but in unconventional aircraft such as canards and those with dual-wings, such as the Quickie, this will not be so. The overall rule stated above must hold, i.e. the neutral point must be aft of the c.g., wherever that may be. The position of the center of gravity is determined by factors such as the positions of loads, e.g. passengers, fuel, weapons, etc.; whether such loads can vary, e.g. presence or absence of luggage, ammunition, etc.; and how fuel is consumed during flight. Additional information regarding the usual position of the neutral point aft of the center of gravity is at longitudinal static stability. (For an aircraft this may be described as positive static margin.) The response of an aircraft or missile to an angular disturbance such as a pitch disturbance is determined by its static margin.In missile analysis, static margin is defined as the distance between the center of gravity and the center of pressure. Missiles are symmetric vehicles and if they have airfoils they too are symmetric. For missiles, positive static margin implies that the complete vehicle makes a restoring moment for any angle of attack from the trim position. If the center of pressure is behind the center of gravity then the moment will be restoring. For missiles with symmetric airfoils, the neutral point and the center of pressure are coincident and the term neutral point is not used.".
- Static_margin wikiPageID "12127040".
- Static_margin wikiPageLength "5865".
- Static_margin wikiPageOutDegree "13".
- Static_margin wikiPageRevisionID "675442392".
- Static_margin wikiPageWikiLink Aerodynamic_center.
- Static_margin wikiPageWikiLink Angle_of_attack.
- Static_margin wikiPageWikiLink Autopilot.
- Static_margin wikiPageWikiLink Category:Aerodynamics.
- Static_margin wikiPageWikiLink Category:Aerospace_engineering.
- Static_margin wikiPageWikiLink Center_of_pressure_(fluid_mechanics).
- Static_margin wikiPageWikiLink Euler_angles.
- Static_margin wikiPageWikiLink Longitudinal_static_stability.
- Static_margin wikiPageWikiLinkText "Static margin".
- Static_margin wikiPageWikiLinkText "static margin".
- Static_margin wikiPageWikiLinkText "static stability".
- Static_margin wikiPageUsesTemplate Template:Reflist.
- Static_margin subject Category:Aerodynamics.
- Static_margin subject Category:Aerospace_engineering.
- Static_margin type Aeronautic.
- Static_margin type Discipline.
- Static_margin type Dynamic.
- Static_margin type Technology.
- Static_margin comment "If an aircraft in flight suffers a disturbance in pitch that causes an increase (or decrease) in angle of attack, it is desirable that the aerodynamic forces on the aircraft cause a decrease (or increase) in angle of attack so that the disturbance does not cause a continuous increase (or decrease) in angle of attack.".
- Static_margin label "Static margin".
- Static_margin sameAs Q7604177.
- Static_margin sameAs هامش_ساكن.
- Static_margin sameAs m.02vqpd3.
- Static_margin sameAs Q7604177.
- Static_margin wasDerivedFrom Static_margin?oldid=675442392.
- Static_margin isPrimaryTopicOf Static_margin.