=
Note: Conversion is based on the latest values and formulas.
aerodynamics - Why is an elliptical wing planform so … On the untwisted elliptical wing the local lift coefficient is constant over span, and changes in angle of attack over the linear range will change the lift coefficient equally everywhere. This, when combined with the elliptical chord distribution over span, means that the circulation distribution will stay elliptical over the linear angle of attack range.
aircraft design - Why does the elliptical wing planform have two ... 17 Nov 2020 · Generally, I have seen that the planform of an elliptical wing consists of two different types of elliptical curves. The elliptical curve towards the leading edge has a lower value for semi-minor axis and the curve towards the trailing edge has a higher value of semi-minor axis. What is the reason for such a geometry? (Image is attached for ...
Spitfire, elliptical wings --- Why? | Aircraft of World War II ... 29 Mar 2009 · Simple explanation - a true elliptical wing planform generated the least possible Induced drag when compared to rectangular or trapezoidal planforms. That being said, wing twist to achieve wing tip control near stall (washout) negated some of the advantages. The Spit designed wing twist into the wing for just that pupose.
Why does the elliptical wing have the lowest drag? 2 Oct 2016 · Only the wing with a constant downwash angle will have the minimum induced drag for a given lift. This is not necessarily an elliptic wing. By selecting the right twist (incidence variation over wingspan), any planform can be made to produce a constant downwash angle, albeit at only one angle of attack.
For the elliptical wing, which property is actually elliptically ... 3 Jul 2017 · The twisted wing has a wing root with a higher AoA, and a wing tip with lower AoA than aircraft AoA: the fat bit of the wing has the higher drag, since wing drag is a function of chord and AoA. So total wing drag of the tapered wing is higher than that of the elliptical wing. The tapered twisted wing rules though, because:
Is elliptical wing superior to the regular profile in term of ... 29 Dec 2018 · As P pbehn notes: Spitfire's wing is expensive because is: a. complicated, b. elliptical & c. constantly changing. A & C are the cost killers. A & C are the cost killers. But that complicate spar allowed the Spitifre Mk. 1 to be light enough for a Merlin E, yet able to be strengthened for a Seafire 47.
Why was the Spitfire's elliptical wing almost uncopied by other ... 26 Apr 2019 · Well the short answer is the elliptical wing was used on a lot more aircraft than this article lets on. The following all used an elliptical wing and there are others too: German Heinkel 112 fighter; German Heinkel 111 bomber; German Heinkel 70; US P35; US P43; Italian Reggiane 2000; Japanese Aichi D3A "Val" dive bomber; British Hawker Tempest
What are the different wing planforms? What are each's … 30 Aug 2015 · Elliptical, tapered, and rectangular are for subsonic speeds. At these speeds, the major issue is induced drag. The rectangular wing is the easiest to build. The elliptical wing has the lowest induced drag. Tapered is a compromise between the two. There are other factors such as stall behavior that influence choice of planform.
Airliner sharp wing tip vs elleptical - Aviation Stack Exchange 29 Feb 2024 · An elliptical lift distribution is not optimal in terms of wing weight. It may also not be optimal in terms of handling qualities, tip stall, flutter, aileron reversal, etc. Modern composite wings also flex a tremendous amount in flight some of this can be planned for, but you still need to design a wing that operates well at off-design conditions, not just at a narrow design point.
aerodynamics - Does an elliptical wing planform have an elliptical … 19 Feb 2020 · However, elliptical lift distribution can also be coaxed by judiciously twisting the wing for a planform that is not geometrically elliptical. Addendum on non-flat span : In the case where the span is not flat, either because it has dihedral or is curved, it has been theoretically demonstrated that a non-flat span can achieve lower induced drag than a flat wing of equal …