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A biplane is a fixed-wing aircraft with two main wings stacked one above the other. The first powered, controlled aeroplane to fly, the Wright Flyer, used a biplane wing arrangement, as did many aircraft in the early years of aviation. While a biplane wing structure has a structural advantage over a monoplane, it produces more drag than a monoplane wing. Improved structural techniques, better materials and higher speeds made the biplane configuration obsolete for most purposes by the late 1930s.

Biplanes offer several advantages over conventional cantilever monoplane designs: they permit lighter wing structures, low wing loading and smaller span for a given wing area. However, interference between the airflow over each wing increases drag substantially, and biplanes generally need extensive bracing, which causes additional drag.

Biplanes are distinguished from tandem wing arrangements, where the wings are placed forward and aft, instead of above and below.

The term is also occasionally used in biology, to describe the wings of some flying animals.


1920s biplane hang glider

In a biplane aircraft, two wings are placed one above the other. Each provides part of the lift, although they are not able to produce twice as much lift as a single wing of similar size and shape because the upper and the lower are working on nearly the same portion of the atmosphere and thus interfere with each other's behaviour. For example, in a wing of aspect ratio 6, and a wing separation distance of one chord length, the biplane configuration will only produce about 20 percent more lift than a single wing of the same planform.[1]

The lower wing is usually attached to the fuselage, while the upper wing is raised above the fuselage with an arrangement of cabane struts, although other arrangements have been used. Either or both of the main wings can support ailerons, while flaps are more usually positioned on the lower wing. Bracing is nearly always added between the upper and lower wings, in the form of interplane struts positioned symmetrically on either side of the fuselage and bracing wires to keep the structure from flexing, where the wings are not themselves cantilever structures.

Advantages and disadvantages

Russian Antonov An-2 biplane from the 1940s

The primary advantage of the biplane over a monoplane is to combine great stiffness with light weight. Stiffness requires structural depth and, where early monoplanes had to have this added with complicated extra bracing, the box kite or biplane naturally has a deep structure and is therefore easier to make both light and strong. A braced monoplane wing must support itself fully, while the two wings of a biplane help to stiffen each other. The biplane is therefore inherently stiffer than the monoplane. Also, the structural forces in the spars of a biplane wing tend to be lower, so the wing can use less material to obtain the same overall strength and is therefore much lighter. A disadvantage of the biplane was the need for extra struts to space the wings apart, although the bracing required by early monoplanes reduced this disadvantage.

The low power supplied by the engines available in the first years of aviation limited aeroplanes to fairly low speeds. This required an even lower stalling speed, which in turn required a low wing loading, combining both large wing area with light weight. A biplane wing of the same area as a monoplane has a smaller span and/or chord, reducing the structural forces and allowing it to be lighter.[2]

Biplanes suffer aerodynamic interference between the two planes when the high pressure air under the top wing and the low pressure air above the lower wing cancel each other out. This means that a biplane does not in practice obtain twice the lift of the similarly-sized monoplane. The farther apart the wings are spaced the less the interference, but the spacing struts must be longer, and the gap must be extremely large to reduce it appreciably. Given the low speed and power of early aircraft, the drag penalty of the wires and struts and the mutual interference of airflows were relatively minor and acceptable factors. As engine power rose after World War One, thick-winged cantilever monoplanes became practical and, with its inherently lower drag and higher speed, and from around 1918 it began to replace the biplane in most fields of aviation.

The smaller biplane wing also allows greater maneuverability. During World War One, this further enhanced the dominance of the biplane and, despite the need for speed, military aircraft were among the last to abandon the biplane form. Specialist sports aerobatic biplanes are still occasionally made.


Wing stagger on a Second World War Fleet Finch primary trainer

Biplanes were originally designed with the wings positioned directly one above the other. Moving the upper wing forward relative to the lower one is called positive stagger or, more often, simply stagger. It can increase lift and reduce drag by reducing the aerodynamic interference effects between the two wings by a small degree, but more often was used to improve access to the cockpit. Many biplanes have staggered wings. Common examples from the 1930s include the de Havilland Tiger Moth, Bücker Bü 131 Jungmann and Travel Air 2000.

It is also possible to place the lower wing's leading edge ahead of the upper wing, giving negative stagger. This is usually done in a given design for structural reasons, or to improve visibility. Examples of negative stagger include the Sopwith Dolphin, Breguet 14 and Beechcraft Staggerwing. However, positive (forward) stagger is the norm.


The space enclosed by a set of interplane struts is called a bay (much as the architectural form is used), hence a biplane or triplane with one set of such struts connecting the wings on each side of the aircraft is a single-bay biplane. This provided sufficient strength for smaller aircraft such as the First World War-era Fokker D.VII fighter and the Second World War de Havilland Tiger Moth basic trainer.

The larger two-seat Curtiss JN-4 Jenny is a two bay biplane, the extra bay being necessary as overlong bays are prone to flexing and can fail. The SPAD S.XIII fighter, while appearing to be a two bay biplane, has only one bay, but has the midpoints of the rigging braced with additional struts; however, these are not structurally contiguous from top to bottom wing. The Sopwith 1½ Strutter has a W shape cabane, however as it does not connect the wings to each other, it does not add to the number of bays.

Large transport and bombing biplanes often needed still more bays to provide sufficient strength. These are sometimes referred to as multi-bay biplanes. A small number of biplanes, such as the Zeppelin-Lindau D.I have no interplane struts and are referred to as being strutless.


Because most biplanes do not have cantilever structures, they require rigging wires to maintain their rigidity. Early aircraft used simple wire (either braided or plain), however during the First World War, the British Royal Aircraft Factory developed airfoil section wire named RAFwire in an effort to both increase the strength and reduce the drag. Four types of wires are used in the biplane wing structure. Drag wires inside the wings prevent the wings from being folded back against the fuselage, running inside a wing bay from the forward inboard corner to the rear outboard corner.[3] Anti-drag wires prevent the wings from moving forward when the aircraft stops and run the opposite direction to the drag wires.[4] Both of these are usually hidden within the wings, and if the structure is sufficiently stiff otherwise, may be omitted in some designs. Indeed many early aircraft relied on the fabric covering of the wing to provide this rigidity, until higher speeds and forces made this inadequate. Externally, lift wires prevent the wings from folding up, and run from the underside of the outer wing to the lower wing root.[5] Conversely, landing wires prevent the wings from sagging, and resist the forces when an aircraft is landing, and run from the upper wing centre section to outboard on the lower wings.[6] Additional drag and anti-drag wires may be used to brace the cabane struts which connect the fuselage to the wings, and interplane struts, which connect the upper and lower wings together.


The much smaller lower wing is apparent in this photo of a Nieuport 17

The sesquiplane is a common variation on the biplane where one wing (usually the lower) has not more than half the surface area of the other.[7] The name means "one-and-a-half wings." The arrangement may reduce interference drag between the wings whilst retaining the biplane's structural advantage. Some designs keep the upper and lower spans nearly equal whilst reducing the lower chord, of which the best known examples are probably the series of Nieuport military aircraft -- from the Nieuport 10 through to the Nieuport 27 which formed the backbone of the Allied air forces from 1915 until 1917, and which were widely copied. The most successful of the copies were the Albatros D.III and D.V, which in turn provided the backbone of the German forces. Between the wars in Europe, the Nieuport-Delage NiD 42/52/62 series, Fokker C.Vd & e, and Potez 25 sesquiplanes served in many air forces, while the Waco Custom Cabin series proved to be a popular general aviation aircraft.


1909 Voisin biplane, with "curtains" connecting the upper and lower wings
Late 1930s Fiat CR.42 with Warren truss interplane struts which reduced the work needed in rigging a biplane

The biplane configuration was developed from the box kite by the Australian Lawrence Hargrave.[8] By 1896 Octave Chanute was flying biplane hang gliders and concluded that the externally braced biplane offered better prospects for powered flight than the monoplane. The biplane Wright Flyer of 1903 became the first successful powered aeroplane.

Throughout the pioneer years, both biplanes and monoplanes were common, but by the outbreak of the First World War biplanes had gained favour after several monoplane structural failures resulted in the RFC's "Monoplane Ban" when all monoplanes in military service were grounded, while the French also withdrew most monoplanes from combat roles and relegated them to training. During the period from 1914 to 1925 most new aircraft were biplanes but from 1917, the Germans began experimenting with a new generation of monoplanes such as the Fokker D.VIII that might have ended the biplane's advantages earlier had the war not ended when it had. The French meanwhile had the Morane-Saulnier AI strut braced parasol monoplane in service. Sesquiplane types, which were biplanes with abbreviated lower wings such as the French Nieuport 17 and German Albatros D.III, offered lower drag than a conventional biplane while being stronger than a monoplane.

As the available engine-power and speed increased, the drag penalty of external bracing increasingly limited aircraft performance. To fly faster, it would be necessary to reduce external bracing to create an aerodynamically clean design. Early cantilever designs were too weak or too heavy. The 1917 Junkers J.I sesquiplane utilized corrugated aluminum for all flying surfaces, with a minimum of struts, but it was slow. The 1918 Zeppelin-Lindau D.I fighter was an all-metal stressed-skin monocoque fully cantilevered biplane but was too late to enter service.

By the 1930s biplanes had reached their performance limits, and monoplanes become increasingly predominant, particularly in continental Europe where monoplanes had been increasingly common from the end of World War I. At the start of World War II, several air forces still had biplane combat aircraft in front line service but they were no longer competitive, and most were used in niche roles, such as training or shipboard operation, until shortly after the end of the war. The British Gloster Gladiator and the Italian Fiat CR.42 biplane fighters were both still operational after 1939.[9] The German Heinkel He 50 and the Soviet Polikarpov Po-2 were both used in the night ground attack role throughout the Second World War, with the latter soldiering on until the Korean War.

Boeing-Stearman Model 75 PT-13D biplane trainer from the 30s and 40s

The British Fleet Air Arm flew Fairey Swordfish torpedo bombers from its aircraft carriers in the anti-submarine warfare role until the end of the war because they could operate from the decks of small escort carriers.

Later biplane trainers included the de Havilland Tiger Moth in the RAF, RCAF and others and the Stampe SV.4, which saw service postwar in the French and Belgian Air Forces. The Stearman PT-13 was widely used by the USAAF and the US Navy operated the Naval Aircraft Factory N3N. In later civilian use in the US, the Stearman became particularly associated with stunt flying such as wing-walking, and with crop dusting, where its compactness worked well at low levels, where it had to dodge obstacles.

Polikarpov Po-2, of which over 20,000 were built by the Soviet Union

Modern biplane designs still exist in specialist roles such as aerobatics and agricultural aircraft with the competition aerobatics role and format for such a biplane well-defined by the mid-1930s by the Udet U 12 Flamingo and Waco Taperwing. The Pitts Special dominated aerobatics for many years after World War II and is still in production.

The vast majority of biplane designs have been fitted with reciprocating engines. Exceptions include the Antonov An-3 and WSK-Mielec M-15 Belphegor, fitted with turboprop and turbofan engines respectively. Some older biplane designs, such as the Grumman Ag Cat are available in upgraded versions with turboprop engines.

The two most produced biplane designs were the 1913 British Avro 504 of which 11,303 were built, and the 1928 Soviet Polikarpov Po-2 of which over 20,000 were built, with the Po-2 being the direct replacement for the Soviet copy of the Avro 504. Both were widely used as trainers.

Ultralight aircraft

Mauro Solar Riser electric-powered ultralight biplane

Although most ultralights are monoplanes, the low speeds and simple construction involved have inspired a small number of biplane ultralights, such as Larry Mauro's Easy Riser (1975-). Mauro also made a version powered with solar cells driving an electric motor--called the Solar Riser. Mauro's Easy Riser was used by "Father Goose", Bill Lishman.[10]

Avian evolution

The feathered dinosaur Microraptor gui glided, and perhaps even flew, on four wings, which may have been configured in a staggered sesquiplane arrangement. This was made possible by the presence of flight feathers on both forelimbs and hindlimbs, with the feathers on the forelimbs opening to a greater span. It has been suggested that the hind limbs could not have opened out sideways but in flight would have hung below and slightly behind the fore limbs.[11]

See also



  1. ^ Dommasch, 1961, p.?
  2. ^ Berriman (1913), Page 26.
  3. ^ Gunston, 2004, p.210
  4. ^ Gunston, 2004, p.51
  5. ^ Gunston, 2004, p.382
  6. ^ Gunston, 2004, p.375
  7. ^ Gunston, 2009, p.606
  8. ^ Wragg, 1974, p.?
  9. ^ Coggins, 2000, p.20
  10. ^ Larry Mauro and Bill Lishman
  11. ^ Chatterjee, 2007, pp.1576-80


  • Berriman, A.E.; Aviation, Methuen, 1913.
  • Chatterjee S, Templin RJ (30 January 2007). "Biplane wing planform and flight performance of the feathered dinosaur Microraptor gui". Proceedings of the National Academy of Sciences of the United States of America. 104 (5): 1576-80. Bibcode:2007PNAS..104.1576C. doi:10.1073/pnas.0609975104. PMC 1780066. PMID 17242354.
  • Coggins, Edward V. (2000). Wings That Stay on. Turner. ISBN 978-1681621760.
  • Dommasch, Daniel O.; Sherby, Sydney S.; Connolly, Thomas F. (1961). Airplane Aerodynamics (3rd ed.). Pitman Publishing. ASIN B003YKT5YK.
  • Gunston, Bill (2009). Cambridge Aerospace dictionary (2nd ed.). Cambridge, UK: Cambridge University Press. p. 606. ISBN 978-0-521-19165-4.
  • Gunston, Bill (2004). The Cambridge Aerospace Dictionary Cambridge. Cambridge University Press. p. 34. ISBN 978-0521841405.
  • Wragg, David W. (1974). Flight before flying. Osprey Publishing. ISBN 978-0850451658.

External links

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