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.
96-587: The Royal Aircraft Factory S.E.5 is a British biplane fighter aircraft of the First World War . It was developed at the Royal Aircraft Factory by a team consisting of Henry Folland , John Kenworthy and Major Frank Goodden . It was one of the fastest aircraft of the war, while being both stable and relatively manoeuvrable. According to aviation author Robert Jackson, the S.E.5 was: "the nimble fighter that has since been described as
192-732: A First World War ace with 21.5 victories. Lambert flew the S.E.5a as an American member of the Royal Flying Corps and the Royal Air Force. The Air Force Museum Foundation also helped buy the aircraft. It is painted to represent an S.E.5e of the 18th Headquarters Squadron, Bolling Field, Washington, D.C., in 1925. Another four original airframes are statically displayed at: the Science Museum , London, UK; Royal Air Force Museum , London, UK; South African National Museum of Military History , Johannesburg, South Africa; and
288-653: 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 often 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
384-412: 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. In a biplane configuration with no stagger from the upper wing to the lower wing,
480-624: A documented jet-kill, as one Lockheed F-94 Starfire was lost while slowing down to 161 km/h (100 mph) – below its stall speed – during an intercept in order to engage the low flying Po-2. Later biplane trainers included the de Havilland Tiger Moth in the Royal Air Force (RAF), Royal Canadian Air Force (RCAF) and others and the Stampe SV.4 , which saw service postwar in the French and Belgian Air Forces. The Stearman PT-13
576-513: A faster and more comfortable successor to the Dragon. 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; however, early cantilever designs were either too weak or too heavy. The 1917 Junkers J.I sesquiplane utilized corrugated aluminum for all flying surfaces, with
672-485: A few S.E.5s were issued to other squadrons due to an acute shortage of the S.E.5a. Deliveries of the S.E.5a suffered from delays due to a shortage of available engines with which to power the type. Due to the shortage of aircraft, there was a very slow initial build-up of new S.E.5a squadrons, which lasted well into 1918. Once the Wolseley Viper -powered model became plentiful, many more units were re-equipped with
768-413: A further 56 aircraft were assembled using already-delivered components. At first, airframe construction outstripped the very limited supply of French-built Hispano-Suiza engines and squadrons earmarked to receive the new fighter had to soldier on with Airco DH 5s and Nieuport 24s until early 1918. The troublesome geared "-8b" model was prone to have serious gear reduction system problems, sometimes with
864-422: 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 . In
960-507: A minimum of struts; however, it was relatively easy to damage the thin metal skin and required careful handling by ground crews. The 1918 Zeppelin-Lindau D.I fighter was an all-metal stressed-skin monocoque fully cantilevered biplane, but its arrival had come too late to see combat use in the conflict. 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
1056-400: A more conventional (and comfortable) seating position. No complaints seem to have been made about the view from the cockpit; in fact, this was often cited as one of the strong points of the type. While pilots, some of whom were initially disappointed with the S.E.5, quickly came to appreciate its strength and fine flying qualities, it was popularly judged to have been underpowered; this failing
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#17328011748001152-726: A number of movies. The Curtiss HS-2L flying boat was used extensively in the war for anti-submarine patrols and was operated from bases in Nova Scotia , France , and Portugal . John Cyril Porte of the Royal Navy and Curtiss worked together to improve the design of the Curtiss flying boats resulting in the Curtiss F5L and the similar Felixstowe F.3 . Curtiss also worked with the United States Navy to develop
1248-464: A retractable underslung radiator. Its performance was little better than the S.E.5a, with the extra drag of the big upper wing offsetting gains from the more streamlined fuselage. The S.E.5b was not considered for production. In January 1919, it was tested with standard S.E.5a wings and in this form survived as a research aircraft into the early twenties. The Royal Aircraft Factory S.E.5 was a conventional tractor biplane fighter aircraft. The fuselage
1344-463: A small degree, but more often was used to improve access to the cockpit. Many biplanes have staggered wings. Common examples include the de Havilland Tiger Moth , Bücker Bü 131 Jungmann and Travel Air 2000 . Alternatively, the lower wing can instead be moved ahead of the upper wing, giving negative stagger, and similar benefits. This is usually done in a given design for structural reasons, or to improve visibility. Examples of negative stagger include
1440-473: A somewhat unusual sesquiplane arrangement, possessing a more substantial lower wing with two spars that eliminated the flutter problems encountered by single-spar sesquiplanes. The stacking of wing planes was suggested by Sir George Cayley in 1843. Hiram Maxim adopted the idea for his steam-powered test rig, which lifted off but was held down by safety rails, in 1894. Otto Lilienthal designed and flew two different biplane hang gliders in 1895, though he
1536-560: Is better known for his monoplanes. By 1896 a group of young men in the United States, led by Octave Chanute , were flying hang gliders including biplanes and concluded that the externally braced biplane offered better prospects for powered flight than the monoplane. In 1903, the Wright Flyer biplane became the first successful powered aeroplane. Throughout the pioneer years, both biplanes and monoplanes were common, but by
1632-663: The American Expeditionary Force to equip already-deployed US Army squadrons, the US Government issued multiple orders to the Curtiss Aeroplane and Motor Company for the manufacture and delivery of around 1,000 S.E.5s to be produced in the United States. However, only one Curtiss-built aircraft would be completed prior to the end of the conflict, after which demand for the S.E.5 had effectively evaporated, production being quickly halted after
1728-572: The Armistice that ended the conflict; some were transferred to various overseas military operators, while a number were also adopted by civilian operators. The S.E.5 ( S cout E xperimental 5 ) was designed by Henry Folland , John Kenworthy and Major Frank Goodden of the Royal Aircraft Factory in Farnborough . It was built around the new 150 hp (112 kW) Hispano-Suiza 8 , a V8 engine that, while providing excellent performance,
1824-660: The Australian War Memorial , Canberra, Australia. Two full-scale replica S.E.5a aircraft were built by Miles Aircraft in 1965 for use in film making and were transferred to the Irish civil aircraft register in 1967 while the two were employed in flying scenes for the 1966 war movie The Blue Max . Three flightworthy reproductions (designated SE5a-1), along with a single static example, were constructed by The Vintage Aviator Limited in New Zealand. According to
1920-536: The Bristol M.1 , that caused even those with relatively high performance attributes to be overlooked in favour of 'orthodox' biplanes, and there was an allegedly widespread belief held at that time that monoplane aircraft were inherently unsafe during combat. Between the years of 1914 and 1925, a clear majority of new aircraft introduced were biplanes; however, during the latter years of the First World War,
2016-613: The Curtiss-Wright Corporation . One of the last projects started by Curtiss Aeroplane was the ambitious Curtiss-Bleecker SX-5-1 Helicopter , a design that had propellers located midpoint on each of the four large rotors that drove the main rotors. This design, while costly and well engineered, was ultimately a failure. Curtiss also operated a flying school at Long Branch Aerodrome in Toronto Township, Ontario , from 1915 to 1917 before being taken over by
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#17328011748002112-589: 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
2208-703: 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. The Antonov An-2 was very successful too, with more than 18,000 built. Although most ultralights are monoplanes,
2304-617: The Lite Flyer Biplane, the Sherwood Ranger , and the Murphy Renegade . 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
2400-669: The Model F trainer flying boat. In 1914, Curtiss had lured B. Douglas Thomas from Sopwith to design the Model J trainer, which led to the JN-4 two-seat biplane trainer (known affectionately as the "Jenny"). The Curtiss Aeroplane and Motor Company worked with the United States' British and Canadian allies, resulting in JN-4 (Can) trainers (nicknamed the "Canuck") being built in Canada. In order to complete large military orders, JN-4 production
2496-625: The Morris Cup race in 1927. An original S.E.5a may be seen at the Shuttleworth Collection at Old Warden , England, UK. This aircraft was originally serial F904 of No. 84 Squadron RAF , then flew as G-EBIA from September 1923 to February 1932. It was stored between 1933 and 1955, before being restored to a flightworthy condition by staff at the Royal Aircraft Establishment and then passed onto
2592-771: The NC-4 , which became the first aircraft to fly across the Atlantic Ocean in 1919, making several stops en route. By the end of World War I, the Curtiss Aeroplane and Motor Company would claim to be the largest aircraft manufacturer in the world, employing 18,000 in Buffalo and 3,000 in Hammondsport, New York . Curtiss produced 10,000 aircraft during that war, and more than 100 in a single week. Peace brought cancellation of wartime contracts. In September 1920,
2688-556: The Nieuport-Delage NiD 42 / 52 / 62 series, Fokker C.Vd & e, and Potez 25 , all serving across a large number of air forces. In the general aviation sector, aircraft such as the Waco Custom Cabin series proved to be relatively popular. The Saro Windhover was a sesquiplane with the upper wing smaller than the lower, which was a much rarer configuration than the reverse. The Pfalz D.III also featured
2784-597: The Royal Aircraft Factory (200), Vickers (2,164) and Wolseley Motors Limited (431). Shortly following the American entry into World War I , plans were mooted for several American aircraft manufacturers to commence mass production of aircraft already in service with the Allied powers, one such fighter being the S.E.5. In addition to an order of 38 Austin-built S.E.5a aircraft which were produced in Britain and assigned to
2880-769: The Royal Flying Corps Canada . Glenn H. Curtiss sponsored the Atlantic Coast Aeronautical Station on a 20-acre tract east of the Newport News boat harbor in the Fall of 1915 with Captain Thomas Scott Baldwin as head. Many civilian students, including Canadians, later became famed World War I flyers. Victor Carlstrom , Vernon Castle , Eddie Stinson and General Billy Mitchell trained here. The school
2976-505: The S.E.5a . The initial models of the S.E.5a differed from late production examples of the S.E.5 only in the type of engine installed – a geared 200 hp Hispano-Suiza 8b , often turning a large clockwise-rotation four-bladed propeller, replacing the 150 hp H.S. 8A model. In total 5,265 S.E.5s were constructed by six manufacturers: Austin Motors (1,650), Air Navigation and Engineering Company (560), Curtiss (1), Martinsyde (258),
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3072-615: The Schneider Cup in two consecutive races, those of 1923 and 1925. The 1923 race was won by U.S. Navy lieutenant David Rittenhouse flying a Curtiss R3C to 177.266 miles per hour (285.282 km/h). Piloted by U.S. Army Lt. Cyrus K. Bettis , a Curtiss R3C won the Pulitzer Trophy on October 12, 1925, at 248.9 miles per hour (400.6 km/h). Thirteen days later, Jimmy Doolittle won the Schneider Trophy in
3168-501: The Sopwith Dolphin , Breguet 14 and Beechcraft Staggerwing . However, positive (forward) stagger is much more common. 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
3264-817: The Western Front before the Camel, there were fewer squadrons equipped with the S.E.5 than with the Sopwith fighter. Together with the Camel, the S.E.5 was instrumental in regaining allied air superiority in mid-1917 and maintaining it for some time, ensuring there was no repetition of " Bloody April " 1917 when losses in the Royal Flying Corps were much heavier than in the Luftstreitkräfte . The S.E.5s remained in RAF service for some time following
3360-476: The Wright Aeronautical to form Curtiss-Wright Corporation. In 1907, Glenn Curtiss was recruited by the scientist Dr. Alexander Graham Bell as a founding member of Bell's Aerial Experiment Association (AEA), with the intent of establishing an aeronautical research and development organization. According to Bell, it was a "co-operative scientific association, not for gain but for the love of
3456-466: The aileron and rudder , whilst adjustment of the elevator trim made it possible to fly in a 'hands off' manner. The S.E.5 was powered by various engines, initially adopting a Hispano-Suiza 8 V8 engine . The Hispano-Suiza engine was advanced for the era, incorporating such features as an aluminium cylinder block with steel liners, dual ignition and forced lubrication that aided cooling; especially compared with contemporary rotary engines , it had
3552-412: The dihedral of the wings in order to increase its manoeuvrability and the removal of the head fairing to increase the pilot's visibility to the rear. James McCudden , an ace pilot and former RFC mechanic, was famous for his prolific fine-tuning of his aircraft in order to produce improved performance from it; McCudden was able to increase the top speed by 9 mph and to raise the service ceiling from
3648-587: The fuselage with the breech inside the cockpit , at a slight upwards angle. Typically, spare magazines for the Lewis gun would have been placed within most of the free space in the cockpit including the forward areas, such as the instrumentation panel. The standard instrument panel included a compass , altimeter , tachometer, oil pressure indicator, airspeed gauge, radiator temperature dial, fuel air pressure indicator, fuel selector, and air exchange; these were somewhat difficult to view due to their low-set position in
3744-419: The lift coefficient is reduced by 10 to 15 percent compared to that of a monoplane using the same airfoil and aspect ratio . 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
3840-403: The ' Spitfire of World War One'". In most respects the S.E.5 had superior performance to the rival Sopwith Camel , although it was less immediately responsive to the controls. Problems with its Hispano-Suiza engine, particularly the geared-output H-S 8B -powered early versions, meant that there was a chronic shortage of the type until well into 1918. Thus, while the first examples had reached
3936-874: The 1976 Anglo-French production Aces High . The 1971 film Zeppelin makes reference to the use of the S.E.5 as a weapon to defend against the German Zeppelins that were attacking Britain during the First World War . The film, however, is set in the fall of 1915, a full year-and-a-half before the S.E. 5 entered squadron service. The dogfight scene near the film's conclusion features S.E.5a replicas. Data from South African National Museum of Military History The Vintage Aviator General characteristics Performance Armament Aircraft of comparable role, configuration, and era Biplane Biplanes offer several advantages over conventional cantilever monoplane designs: they permit lighter wing structures, low wing loading and smaller span for
Royal Aircraft Factory S.E.5 - Misplaced Pages Continue
4032-514: The CR.42 was able to achieve success in the defensive night fighter role against RAF bombers that were striking industrial targets throughout northern Italy. The British Fleet Air Arm operated the Fairey Swordfish torpedo bomber from its aircraft carriers, and used the type in the anti-submarine warfare role until the end of the conflict, largely due to their ability to operate from
4128-477: The Camel's two, but it also had a wing-mounted Lewis gun fitted on a Foster mounting , which enabled the pilot to fire at an enemy aircraft from below. This armament configuration was much appreciated by the pilots of the first S.E.5 squadrons as the new hydraulic-link "C.C." synchronising gear for the Vickers machine gun was unreliable at first. The Vickers gun was mounted on the forward left dorsal surface of
4224-528: The Caribou , performed the first non-stop flight between the Canadian mainland and Britain in 30 hours 55 minutes, although the intended target for this long distance flight had originally been Baghdad , Iraq . Despite its relative success, British production of the Dragon was quickly ended when in favour of the more powerful and elegant de Havilland Dragon Rapide , which had been specifically designed to be
4320-695: The Curtiss Aeroplane Company of Hammondsport, New York , and Curtiss Motor Company of Bath, New York . Burgess Company of Marblehead, Massachusetts , became a subsidiary in February 1916. At the same time, the Curtiss Engineering Company was established as a subsidiary in Garden City, New York . With the onset of World War I , military orders rose sharply, and Curtiss needed to expand quickly. In 1916,
4416-425: The Curtiss Aeroplane and Motor Company underwent a financial reorganization and Glenn Curtiss cashed out his stock in the company for $ 32 million and retired to Florida . He continued as a director of the company but served only as an advisor on design. Clement M. Keys gained control of the company from Willys-Overland and it later became the nucleus of a large group of aviation companies. Curtiss seaplanes won
4512-515: 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. Anti-drag wires prevent
4608-577: The French Nieuport 17 and German Albatros D.III , offered lower drag than a conventional biplane while being stronger than a monoplane. During the Interwar period , numerous biplane airliners were introduced. The British de Havilland Dragon was a particularly successful aircraft, using straightforward design to could carry six passengers on busy routes, such as London-Paris services. During early August 1934, one such aircraft, named Trail of
4704-661: The Germans had been experimenting with a new generation of monoplanes, such as the Fokker D.VIII , that might have ended the biplane's advantages earlier had the conflict not ended when it had. The French were also introducing the Morane-Saulnier AI , a strut-braced parasol monoplane , although the type was quickly relegated to the advanced trainer role following the resolution of structural issues. Sesquiplane types, which were biplanes with abbreviated lower wings such as
4800-519: The Imperial Gift in 1919, and the type went on to be the newly formed R.A.A.F.’s main fighter type until the late 1920’s. A number of machines found roles in civilian flying after the war. On 30 May 1922, the first use of skywriting for advertising occurred when Cyril Turner, a former RAF officer, spelt out "London Daily Mail " in black smoke from an S.E.5a at The Derby . Others were used for air racing ; one such privately owned aircraft won
4896-532: The Navy , pressured the industry to form a cross-licensing organization (in other terms a Patent pool ), the Manufacturer's Aircraft Association . Later that year, Curtiss was acquired by the automobile manufacturer Willys-Overland . Curtiss was instrumental in the development of U.S. Naval Aviation by providing training for pilots and providing aircraft. The first major order was for 144 various subtypes of
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#17328011748004992-416: The S.E.5 as "arguably the best British-built fighter of World War I". In March 1917, the S.E.5 entered service with No. 56 Squadron RFC , although the squadron did not deploy to the Western Front until the following month. Everyone was suspicious of the large "greenhouse" windscreens fitted to the first production models. These were designed to protect the pilot in his unusually high seating position, which
5088-472: The S.E.5: "It was very fine to be in a machine that was faster than the Huns, and to know that one could run away just as things got too hot." Sholto Douglas who commanded No. 84 Squadron RFC which was initially equipped with the S.E.5a, listed the type's qualities as being: "Comfortable, with a good all-round view, retaining its performance and manoeuvrability at high level, steady and quick to gather speed in
5184-620: The Shuttleworth Collection. An extensive refurbishment of this aircraft was performed in 2007. It has been re-registered as G-EBIA , it was first painted as D7000 , then as F904 . An original S.E.5e may be seen in the National Museum of the United States Air Force at Dayton , Ohio, USA. The museum acquired the S.E.5e through a donation by the estate of Lt. Col. William C. Lambert , USAF Ret,
5280-522: The advantage of being easy to operate by most pilots. An expansion tank for the cooling system was integrated into the leading edge of the upper wing's centre section. One of its greatest advantages over the Sopwith Camel was its superior performance at altitude, making it a much better match for the Fokker D.VII when that fighter arrived at the front. The S.E.5 was armed with a single synchronised .303 -inch Vickers machine gun in contrast to
5376-602: The art and doing what we can to help one another." In 1909, shortly before the AEA was disbanded, Curtiss partnered with Augustus Moore Herring to form the Herring-Curtiss Company . It was renamed the Curtiss Aeroplane Company in 1910 and reorganized in 1912 after being taken over by the Curtiss Motor Company. The Curtiss Aeroplane and Motor Company was created on January 13, 1916, from
5472-407: The biplane naturally has a deep structure and is therefore easier to make both light and strong. Rigging wires on non-cantilevered monoplanes are at a much sharper angle, thus providing less tension to ensure stiffness of the outer wing. On a biplane, since the angles are closer to the ideal of being in direct line with the forces being opposed, the overall structure can then be made stiffer. Because of
5568-427: The cockpit. According to "Dodge" Bailey, Chief Test Pilot of the Shuttleworth Collection , the S.E.5's cockpit was "the best of the bunch from the era". It was set amidships, making it difficult to see over the long front fuselage, but otherwise visibility was good. Individual in-service S.E.5s would often receive customisations and user-specified tweaks at the request of their pilots. Popular changes included reducing
5664-439: The company moved its headquarters and most manufacturing activities to Buffalo, New York , where there was far greater access to transportation, manpower, manufacturing expertise, and much needed capital. The company housed an aircraft engine factory in the former Taylor Signal Company-General Railway Signal Company . An ancillary operation was begun in Toronto, Ontario, that was involved in both production and training, setting up
5760-498: 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
5856-412: The dive, capable of a very fine zoom, useful in both offence and defence, strong in design and construction, [and] possessing a reliable engine". Soon after the Armistice the S.E.5a was withdrawn from RAF service. It was retained for a time in Canada, and in 1921 a Viper-engined S.E.5a was taken to Japan by the British Aviation Mission to the Imperial Japanese Navy . Australia received 35 S.E.5a under
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#17328011748005952-470: The drag from the number of struts used. The structural forces acting on the spars of a biplane wing tend to be lower as they are divided between four spars rather than two, so the wing can use less material to obtain the same overall strength and is therefore lighter. A given area of wing also tends to be shorter, reducing bending moments on the spars, which then allow them to be more lightly built as well. The biplane does however need extra struts to maintain
6048-484: 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 biplane, the Italian Fiat CR.42 Falco and Soviet I-153 sesquiplane fighters were all still operational after 1939. According to aviation author Gianni Cattaneo,
6144-407: The first flying school in Canada in 1915. In 1917, the two major aircraft patent holders, the Wright Company and the Curtiss Company, had effectively blocked the building of new airplanes , which were desperately needed as the United States was entering World War I . The U.S. government, as a result of a recommendation of a committee formed by Franklin D. Roosevelt , then Assistant Secretary of
6240-416: The gap between the wings, which add both weight and drag. 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. Obtaining a large enough wing area without the wings being long, and thus dangerously flexible
6336-480: The group, the reproduction aircraft, which was the company's first project, combined some authentic components, such as the Hispano engines used, with newly-fabricated parts based on original archived drawings. The Museum of Flight in Seattle , Washington , US displays the reproduction SE.5a that Bobby Strahlman and his partners completed for collector Doug Champlin in 1989. This reproduction features one .303 Vickers and one .303-calibre Lewis machine gun, and carries
6432-435: The hind limbs could not have opened out sideways but in flight would have hung below and slightly behind the fore limbs. Curtiss Aeroplane and Motor Company Curtiss Aeroplane and Motor Company (1909–1929) was an American aircraft manufacturer originally founded by Glenn Hammond Curtiss and Augustus Moore Herring in Hammondsport, New York . After significant commercial success in its first decades, it merged with
6528-424: 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 . Other biplane ultralights include the Belgian-designed Aviasud Mistral , the German FK12 Comet (1997–),
6624-519: 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. The primary advantage of the biplane over a monoplane is its ability to combine greater stiffness with lower weight. Stiffness requires structural depth and where early monoplanes had to have this provided with external bracing,
6720-453: The most famed copies was the Siemens-Schuckert D.I . The Albatros D.III and D.V , which had also copied the general layout from Nieuport, similarly provided the backbone of the German forces during the First World War. The Albatros sesquiplanes were widely acclaimed by their aircrews for their maneuverability and high rate of climb. During interwar period , the sesquiplane configuration continued to be popular, with numerous types such as
6816-422: The night ground attack role throughout the Second World War. In the case of the Po-2, production of the aircraft continued even after the end of the conflict, not ending until around 1952. A significant number of Po-2s were fielded by the Korean People's Air Force during the Korean War , inflicting serious damage during night raids on United Nations bases. The Po-2 is also the only biplane to be credited with
6912-486: 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. Figures such as aviation author Bruce observed that there was an apparent prejudice held even against newly-designed monoplanes, such as
7008-596: The paint scheme of American ace George Vaughn who served with the Royal Flying Corps. The SE.5 was displayed at Champlin's fighter museum at Mesa , Arizona , US until the collection was transferred to Seattle in 2003. The Royal Aircraft Factory S.E.5 has been portrayed, both by original and replica aircraft, in various movies. These include Wings (1927), Hell's Angels (1930), Flying Down to Rio (1933), Crimson Romance (1934), Test Pilot (1939) and The Aviator (2004). Converted Stampe et Vertongen SV.4 trainer/tourer aircraft were used to portray S.E.5s in
7104-486: The period. While the S.E.5 was not as agile and effective in a tight dogfight as the Camel it was much easier and safer to fly, particularly for novice pilots. According to "Dodge" Bailey, the former Chief Test Pilot of the Shuttleworth Collection , it had "somewhat similar handling characteristics to a de Havilland Tiger Moth , but with better excess power". Only 79 original S.E.5 aircraft had been completed prior to production settling upon an improved model, designated as
7200-466: The propeller (and even the entire gearbox on a very few occasions) separating from the engine and airframe in flight, a problem shared with the similarly-powered Sopwith Dolphin . The introduction of the 200 hp (149 kW) Wolseley Viper , a high-compression, direct-drive version of the Hispano-Suiza 8a made under licence by Wolseley Motors Limited , solved the S.E.5a's engine problems and
7296-424: The reduced stiffness, wire braced monoplanes often had multiple sets of flying and landing wires where a biplane could easily be built with one bay, with one set of landing and flying wires. The extra drag from the wires was not enough to offset the aerodynamic disadvantages from having two airfoils interfering with each other however. Strut braced monoplanes were tried but none of them were successful, not least due to
7392-657: The relatively compact decks of escort carriers . Its low stall speed and inherently tough design made it ideal for operations even in the often severe mid-Atlantic weather conditions. By the end of the conflict, the Swordfish held the distinction of having caused the destruction of a greater tonnage of Axis shipping than any other Allied aircraft. Both the German Heinkel He 50 and the Soviet Polikarpov Po-2 were used with relative success in
7488-544: The same aircraft fitted with floats with a top speed of 232.573 miles per hour (374.290 km/h). The Curtiss Robin light transport was first flown in 1928, becoming one of the company's biggest sellers during the Great Depression , and the 769 built helped keep the company solvent when orders for military aircraft were hard to find. On July 5, 1929, Curtiss Aeroplane and Motor Company together with 11 other Wright and Curtiss affiliated companies merged to become
7584-675: The series of Nieuport military aircraft—from the Nieuport 10 through to the Nieuport 27 which formed the backbone of the Allied air forces between 1915 and 1917. The performance of the Nieuport sesquiplanes was so impressive that the Idflieg (the German Inspectorate of flying troops) requested their aircraft manufacturers to produce copies, an effort which was aided by several captured aircraft and detailed drawings; one of
7680-506: The squarer wings also gave much improved lateral control at low airspeeds. Like the other significant Royal Aircraft Factory aircraft of the war ( B.E.2 , F.E.2 and R.E.8 ) the S.E.5 was inherently stable, making it an excellent gunnery platform, but it was also quite manoeuvrable. It was one of the fastest aircraft of the war at 138 mph (222 km/h), equal at least in speed to the SPAD S.XIII and faster than any standard German type of
7776-437: The standard 17,000 ft to 20,000 ft. His adaptions included replacing the standard pistons with high compression versions, shortening the exhaust (saving weight and improving exhaust scavenging), and changes to mixture, ignition and other engine settings as well as fitting a salvaged German propeller spinner (which he himself credited as gaining 3 mph alone). Aviation authors Donald Nijboer and Dan Patterson describe
7872-415: The structural problems associated with monoplanes, but offered little improvement for biplanes. The default design for a biplane has 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
7968-670: 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. As engine power and speeds rose late in World War I , thick cantilever wings with inherently lower drag and higher wing loading became practical, which in turn made monoplanes more attractive as it helped solve
8064-494: The type. By the end of the war, the S.E.5a was employed by a total of 21 British Empire squadrons as well as two U.S. units. Many of the top Allied aces of the Great War flew this fighter, including Billy Bishop , Andrew Beauchamp-Proctor , Edward Mannock and James McCudden . Legendary British ace Albert Ball was initially disparaging of the S.E.5, but in the end claimed 11 of his 44 victories flying it. McCudden wrote of
8160-400: The upper and lower wings together. The sesquiplane is a type of biplane where one wing (usually the lower) is significantly smaller than the other. The word, from Latin, means "one-and-a-half wings". The arrangement can reduce drag and weight while retaining the biplane's structural advantages. The lower wing may have a significantly shorter span, or a reduced chord . Examples include
8256-434: The wings from folding up, and run from the underside of the outer wing to the lower wing root. 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. 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
8352-421: The wings from moving forward when the aircraft stops and run the opposite direction to the drag wires. 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
8448-409: Was a wire-braced box girder structure while the wings were furnished with wooden spars and internal ribs . The fuselage was narrower than many contemporary aircraft, which provided the pilot with good all-round visibility. The aircraft had considerable structural strength, which was credited with improving the type's crashworthiness and survivability. It could also withstand high-g manoeuvres and
8544-407: Was addressed by the introduction of the more powerful S.E.5a. In June 1917, the S.E.5a entered service and quickly began to replace the S.E.5. At this time 56 Squadron was still the only unit flying the new fighter; in fact it was the only operational unit to be fully equipped with the initial 150 hp S.E.5 – all other S.E.5 squadrons officially used the 200 hp S.E.5a from the outset – although
8640-485: Was distributed to five other manufacturers. After the war, large numbers of JN-4s were sold as surplus, making influential as the first plane for many interwar pilots, including Amelia Earhart . A stamp was printed to commemorate the Curtiss JN-4 , however a printing error resulted in some having the aircraft image inverted, which has become very valuable, and one of the best known rare stamps, even being featured in
8736-408: Was in turn intended to improve vision over the upper wing. The squadron did not fly its first patrol with the S.E.5 until 22 April, by which time, on the insistence of Major Blomfield, 56 squadron's commanding officer, all aircraft had been fitted with small rectangular screens of conventional design. The problem of the high seating position was solved by simply lowering it, pilots in any case preferring
8832-554: Was initially underdeveloped and unreliable. The first of three prototypes flew on 22 November 1916. The first two prototypes were lost in crashes (the first killing the chief test pilot at the Royal Aircraft Factory, Major Frank Goodden, on 28 January 1917) due to a weakness in their wing design. The third prototype underwent modification before production commenced; the S.E.5 was known in service as an exceptionally strong aircraft which could be dived at very high speed –
8928-404: Was more readily accomplished with a biplane. The smaller biplane wing allows greater maneuverability . Following World War I, this helped extend the era of the biplane and, despite the performance disadvantages, most fighter aircraft were biplanes as late as the mid-1930s. Specialist sports aerobatic biplanes are still made in small numbers. Biplanes suffer aerodynamic interference between
9024-402: Was promptly adopted as the type's standard powerplant. A number of aircraft were subsequently converted to a two-seat configuration in order to serve as trainer aircraft . The S.E.5b was a variant of the S.E.5 with a streamlined nose and upper and lower wings of different span and chord. The single example, a converted S.E.5a, first flew in early April 1918. It had a spinner on the propeller and
9120-489: Was relatively resistant to battle-damage. Unlike many of its peers, which were highly agile but unforgiving, the S.E.5 was comparatively stable and easy to fly; its stability enabling pilots to more readily fire upon enemies from further away with a greater degree of accuracy. It had a noticeably lower accident rate than comparable aircraft. The exception to its generally stability was an excessive amount of adverse yaw . The yaw could be compensated for by balanced application of
9216-777: Was widely used by the United States Army Air Force (USAAF) while 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. Modern biplane designs still exist in specialist roles such as aerobatics and agricultural aircraft with
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