This article is about the term as used in aviation. For its general use, see
Plan view.
In aviation, a planform is the shape and layout of a fixed-wing aircraft's fuselage and wing. Of all the myriad planforms used, they can typically be grouped into those used for low-speed flight, found on general aviation aircraft, and those used for high-speed flight, found on many military aircraft and airliners.
The planform may also refer to the projected area of the wing. From a top view perspective, one can extend the lines from the leading and trailing edges on the left and right side of the fuselage until they meet at the centerline of the aircraft. The area of the wing along with this projected area is commonly refereed to as the planform area, Failed to parse (Missing texvc executable; please see math/README to configure.): S_{ref} . It is used as a non-dimensionalization parameter.
Straight wing |
Swept wing |
Variable sweep wing |
Delta wing (tailless) |
A
Spitfire built in 1945 shows off its elliptical planform
The primary concern in low speed flight is the aspect ratio, the comparison of the length of the wing measured out from the fuselage, wingspan, compared to the length from front to back, chord. Wings with higher aspect ratios, that is, wings that are longer and skinnier, have lower drag for any given amount of lift than a wing of the same area that is shorter and fatter. This is due to an effect known as induced drag, caused by airflow around the tip of the wing. As the size of the tip decreases compared to the wing's overall size, the magnitude of the induced drag is reduced.
This is why designers of gliders, who want a high lift to drag ratio, use very long and skinny high aspect ratio wings and winglets. At higher speeds, however, different forms of drag become more prominent, meaning that the large aspect ratio wings found on gliders become very inefficient. Another issue is strength; it is harder to build a longer wing with sufficient stiffness than a short one.
There are other ways to reduce induced drag, mostly by changing the shape of the wing to reduce the size of the tip. The elliptical wing found on the Supermarine Spitfire and Republic P-47 is the most efficient, but difficult to build. A practical compromise is to taper the wing towards the tip, a feature that can be found on almost all modern aircraft (including gliders).
At higher speeds nearing the speed of sound, a new form of drag appears: wave drag. Wave drag is considerably more powerful than induced drag, and must be avoided at all costs to improve performance. Doing so demands a wing that is as thin as possible, with a slowly changing profile over a wide chord. Of course, this is basically the opposite goal to low speed wings, which presents a problem.
Just as on the lower speed designs, making an ideal high speed planform is difficult for practical reasons. In this case, a very thin wing makes it difficult to use the internal room to store fuel and landing gear, makes the wing far less stiff torsionally, and causes increased induced drag when flying slower.
Solutions to this problem come in many forms, notably the use of the swept wing and delta wing, both of which avoid the shock wave at the leading edge. Other designs make the wing as thin as possible, leading to designs like the F-104 Starfighter.
-
Douglas Dakota. It is unusual for a piston-engine airplane to have swept leading edges and straight trailing edges
-
-
-
-
![Planform view of a British Airways 767-300 after takeoff. The 767 has been produced in three fuselage lengths.[22] These debuted in progressively larger form as the 767-200, 767-300, and 767-400ER, respectively.](http://web.archive.org./web/20121027212921/http://cdn9.wn.com/pd/d5/4d/efb9b79fed762f03d3da56485294_medium.jpg "Planform view of a British Airways 767-300 after takeoff. The 767 has been produced in three fuselage lengths.[22] These debuted in progressively larger form as the 767-200, 767-300, and 767-400ER, respectively.")
.jpg)
