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2007-01-22 02:36:00 · 15 answers · asked by ? 2 in Cars & Transportation Aircraft

15 answers

Dihedral is the upward angle from horizontal in a fixed-wing aircraft or bird wing from root to tip, as viewed from directly in front or behind the aircraft. Downward angled wings have negative dihedral, or anhedral. Wings with local dihedral angles that change along the span are polyhedral.

The purpose of positive dihedral is to confer stability in the roll axis. Most aircraft in the civilian or transport sector use dihedral for roll stability. The dihedral angle is usually greater on low-wing aircraft, compared to an otherwise similar high-wing aircraft.

2007-01-22 02:40:26 · answer #1 · answered by Anonymous · 3 0

Dihederal has no effect on an aircraft whatsoever other than increase its stability in the roll axis. Model aircraft that do not have ailerons normally have a greater dihedral angle than aircraft with full control. Sighted from the end on the aircraft, in straight and level flight, the same area on wing is presented to the earth. If the aircraft rolls, the angle of the outer wings increase and the inner wing decreases and, therefore presents a greater wing area to the earth. This apparent increase will increase the lift on that the side, so righting the aircraft and putting it back onto an even keel.

2007-01-23 04:53:21 · answer #2 · answered by Anonymous · 0 0

Dihedral increases the normal-attitude roll stability of an aircraft, that is to say the ability of the aircraft to right itself after a roll without any control input.

It has a secondary effect of increasing induced drag because the change in lift angle of the wing requires an increase in overall lift to maintain flight.

Cheers.

2007-01-22 02:50:40 · answer #3 · answered by chopchubes 4 · 0 0

The dihedral of the wings increases directional stability of the aircraft. It is not as noticeable on high-wing aircraft as it is on low wing aircraft because high wing aircraft are much more stable due to the center of gravity being underneath the center of lift.

A very few, primarily acrobatic and military fighters, employ a cathedral, in which the wings slope downward from the fuselage to the tip, promoting instability and making the aircraft much more manueverable, but a bit of a handful to hand-fly.

2007-01-22 08:07:53 · answer #4 · answered by jettech 4 · 0 0

Dihedral is the upward bend of the wings or wingtips. You can see this in nature on turkey buzzards and other soaring birds.

Airplanes with noticeable dihedral in their wings are sailplanes, the F4 Phantom, F4U Corsair and A10 Warthog.

Dihedral makes the wing & aircraft more stable, especially at slower speeds. It does this two ways. One by allowing more air to slip laterally across the wing surface to the outsides, in a way imitating the effect of wing sweep. Second by raising the lifting point of the wing higher than the rest of the wing and higher than the mounting point on the fuselage. This wing design does compromise some lift, but this is minor & usually compensated for by increasing wing area. Sacrificing some lift for stability is not a bad thing.

To illustrate this point, take two low-winged model airplanes - one with flat wings and another with a large amount of dihedral. Suspend them by strings at the wingtips and you may notice that the flat winged airplane tries to tip up or down more easily.

There are also planes with negative dihedral, such as the AV8B Harrier. These wings are usually mounted high on the fuselage and it gives greater lift and more responsive handling, but at the cost of stability. An example is listed below...

In the case of the Harrier, the extreme downward tilt of the wings helps bring the wingtip wheels closer to the landing surface, facilitate easier weapons loading and trap more air under the aircraft during it's vertical takeoff manuever.

2007-01-22 02:46:13 · answer #5 · answered by Anonymous · 2 0

No, there is not any raise benefit. Anhedral is a stability reducer. A extreme wing placement, universal on heavy raise plane as a manner to allow for a short touchdown equipment and to that end low floor point on the same time as offering the mandatory clearance for the engines, is resembling some degree of dihedral. Sweepback, used in extreme velocity airplane to put off the onset of transonic circulate (the place drag will improve by way of elementary ask your self) additionally provides a level of equivalent dihedral; the effect of the two extreme wing and sweepback is oftentimes too lots dihedral. some dihedral is solid because it factors lateral stability; yet too lots of it skill the plane could be difficult to regulate because it does no longer desire to alter from its contemporary mindset. So, some anhedral is put in the wing to make the plane greater maneuverable (and much less stubbornly solid).

2016-12-16 10:35:52 · answer #6 · answered by ? 4 · 0 0

Dihedral increases the dynamic stability of an aircraft, especially at low speeds. Most planes that fly at speeds below the speed of sound will have a dihedral, while most aircraft that can fly above the speed of sound will have an anhedral (meaning wings that slope downwards) because the speed at which they fly will impart the necessary stability.

2007-01-23 19:04:48 · answer #7 · answered by RaviAsrani 2 · 0 0

I thought the dihedral on airliners was "variable". Variable in the sense that the angle at the wingroot is slightly steeper than the angle at the wingtip...as you move from the wingroot to the wingtip, the angle decreases. I've always thought that this angle not only provides stability but also provides an optimum level of lift while keeping drag to a desireable minimum while having the aircraft pose at a passenger-friendly angle-of-attack or nose pitch while flying (also good for keeping one's "Specific Fuel Consumption" low).

2007-01-24 02:25:15 · answer #8 · answered by Fulani Filot 3 · 0 0

Dihedral enhances positive stability around the longitudinal axis. That is: The tendency for the aircraft to return to wings-level after a small roll force has been applied to it.

2007-01-22 06:48:32 · answer #9 · answered by Jason 5 · 0 0

The upward slope of an aircraft's wing.

2007-01-22 02:41:05 · answer #10 · answered by rusco21 3 · 0 0

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