Examples of 'swept wing' in a sentence
Meaning of "swept wing"
A swept wing is a design feature commonly used in aviation, particularly in the design of aircraft wings. It refers to the shape of the wing where the leading edge is angled backward relative to the fuselage. This design helps improve aerodynamics, reduces drag, and enhances the maneuverability of the aircraft
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- A wing that is angled backwards (or, occasionally, forwards) from its point of attachment to the fuselage, so that the wingtip is located further aft or forward than the wing root.
- Alternative form of sweptwing
How to use "swept wing" in a sentence
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swept wing
How do you determine the area of a swept wing.
The swept wing also has several more problems.
Forward swept wing.
The swept wing is already an indirect application of the area rule.
The original design would have had a slightly swept wing.
The airflow over a swept wing encounters the wing at an angle.
The same basic layout is desirable for an aircraft with a swept wing as well.
Its lightweight swept wing design makes it extremely maneuverable and agile.
Its wing design comes from the moderately swept wing of the Citation Sovereign.
Its swept wing has metal spars and ailerons but wooden ribs.
Later, experimental aircraft were built to study the effects of a simple swept wing.
Stall behaviour of the swept wing was also poorly understood and could be extremely sharp.
The JetStar has a fairly typical business jet design layout, with a swept wing and a cruciform tail.
Swept wing aircraft will also experience wing twist as a geometric result of the thermal bending.
The mechanism for varying the angle of a swept wing is complicated, heavy and expensive.
See also
A swept wing has a lower, flatter curve with a higher critical angle.
The Hunter is a conventional swept wing all-metal monoplane.
However, the swept wing was found to be unsatisfactory with poor aileron authority.
Unlike the earlier Mirage III the F2 had a high-mounted swept wing and horizontal tail surfaces.
As a swept wing deflects in a downward direction, the wing will twist in a nose-up direction.
In line with the fourth chord, the swept wing is 25 degrees.
While a swept wing is stable in straight flight, it still experiences adverse yaw during a turn.
Adolf Busemann introduced the concept of the swept wing and presented this in 1935 at the 5.
It was a swept wing tandem two-seater, with a pusher configuration engine and twin-boom fuselage.
Blohm & Voss had been studying the swept wing and its associated problems such as aeroelasticity.
One limiting factor in swept wing design is the so-called "middle effect.
The aircraft had a 50° swept wing fitted with air brakes and boosted controls.
