Share on Facebook Share on Twitter Email
Answers.com

glider

 
(glī'dər) pronunciation
n.
  1. A light engineless aircraft designed to glide after being towed aloft or launched from a catapult.
  2. A swinging couch suspended from a vertical frame.
  3. A device that aids gliding.

Search unanswered questions...
Enter a question here...
Search: All sources Community Q&A Reference topics

Nonpowered heavier-than-air craft capable of sustained flight. Early experimenters in glider flight included George Cayley, who built the first man-carrying glider in 1853, and Otto Lilienthal (1848 – 1896), who introduced tail stabilizers on his first practical man-carrying craft in 1891. Improvements by Octave Chanute (1832 – 1910) in 1896 and by Wilbur and Orville Wright in 1902 perfected the control needed for developing the Wrights' powered airplane in 1903. The slender-winged glider was launched by being towed behind an airplane or a car. Gliders were used in World War II to carry troops. Today they are mainly used for recreation; the sailplane type is built for soaring on the lift from thermals. See also hang gliding.

For more information on glider, visit Britannica.com.

An unpowered flying device that attempts to copy the flight of soaring birds. In October 1911, Orville Wright made a gliding flight of nearly 10 min duration, and demonstrated that gliders could stay up for long periods in rising air. This condition of flight, called slope soaring, was the basic method of soaring flight until about 1930. Thermal soaring, the next step, was accomplished by flying in areas of rising convection currents. By the use of thermal flight, the modern glider can fly almost anywhere in the world for extended time and distances over 500mi (800 km) in one flight. Other methods of soaring make use of clouds and standing-wave phenomena in the atmosphere. High-performance gliders (sailplanes) may be launched by towing behind powered aircraft or by car towing, which is used to a lesser extent. Some gliders have been fitted with a small motor and propeller, which enables them to take off and climb to an altitude where rising air permits them to soar unpowered.

Sailplane construction traditionally has been of wood and plywood, although the use of aluminum alloy has become common. The use of fiber glass as primary structure has also come into prominence, since it is possible to produce the external shapes in accurate molds with greater precision, resulting in improved performance.

Modern foot-launched hang gliders with aluminum tube frames have flown over 100 mi (160 km) in straight-line distance, have reached about 20,000 ft (6000 m) altitude, and have remained aloft more than 15 h. But it is not so much their performance that makes hang gliders popular, but their low cost, their convenience of folding into a small package for transport or storage, and the fact that no license is required for glider or pilot.


Gliders first saw military use during WW II and were used by Axis and Allied forces for the movement of troops, heavy weapons, and equipment. The Germans were the first to use gliders operationally, having developed them during the period 1933-7. The DFS 230 entered service in 1940 as the standard cargo- and troop-carrier, accommodating ten troops including the pilot. Comprising a tubular steel frame covered with fabric and wooden wings, it was normally towed by a Junkers Ju 52, Heinkel He 111, Henschel 126, Messerschmitt Bf 110, or Junkers Ju 87, at speeds of up to 120 mph (193 km/ph). The DFS 230 was used to particularly good effect during the assault on Eben Emael in May 1940 when nine gliders carrying a handful of engineers landed on the top of the fortress whose 5 foot (1.52 metre) thick reinforced concrete casemates were then breached with hollow charge explosives.

The DFS 230 saw action again in May 1941 when 71 gliders landed elements of the 1st Battalion of XI Air Corps' Assault Regiment on Crete. A large number of gliders were destroyed during the landings, which took place under heavy fire, while others suffered damage from the rocky terrain on which they landed.

In mid-1941 a partial replacement for the DFS 230, the Gotha 242, entered service. With a wingspan of 79 feet (24.08 metres) and payload of 8, 000 lb (3, 629 kg), it could carry 23 troops, a field gun, and light vehicle. Its construction comprised a nacelle of fabric-covered tubular steel with twin tail booms and wings of wood. With a maximum towing speed of 180 mph (290 km/ph), it was towed by a Junkers 52 or Heinkel 111.

In 1941 the Luftwaffe introduced the Me 321 ‘Gigant’. With a wingspan of 181 feet (55.2 metres), its payload was 28 tons of cargo or 200 troops. The fuselage was of fabric-covered tubular steel and the wings of tubular steel were covered with plywood and fabric. Take-off was assisted by rockets in racks under the wings. A special five-engined tug aircraft, the Heinkel 111Z, was developed to tow this glider. A powered version of the Me 321, the Me 323, entered service in 1942. Equipped with six engines and a wingspan of 181 feet (55.2 metres), it could carry up to 21, 500 lb (9, 752.4 kg) of cargo, an 88 mm gun, or 130 troops.

The first British glider to enter service was the Hotspur. Flown by a crew of two, it was, however, capable of carrying only eight troops or approximately 1 ton of cargo. Thus, shortly after entering service, it was relegated to use as a trainer. The workhorse of British airborne forces was the Horsa which was also used by US airborne divisions. Constructed of plywood with a fabric skin, it had a wingspan of 88 feet (26.8 metres) and a crew of two. Towed by a Stirling or Halifax bomber, or Dakota, it had a maximum towing speed of 160 mph (257 km/ph). With a payload of 3.5 tons, it could carry 28 troops, a jeep and trailer or 6-pounder anti-armour gun, or a 75 mm pack howitzer and jeep.

In 1941, the Hamilcar entered service. Constructed of wood and metal, with a wingspan of 110 feet (33.5 metres) and a payload of 17, 500 lb (7, 938 kg), it was designed to carry heavy loads: 17-pounder anti-armour gun and tractor; 25-pounder field gun and tractor; a light tank or two Bren carriers. With a crew of two, it was towed by either a Stirling or Halifax bomber and had a maximum towing speed of 150 mph (241 km/ph).

The first operational use of gliders by the British took place in November 1942 when 34 engineers from 1st Airborne Division were flown to Norway in two Horsas of the 1st Battalion The Glider Pilot Regiment, towed by Halifax tugs of 38 Wing RAF. Their mission was to attack the Norsk Hydro Plant at Vermork, in southern Norway, which produced heavy water for the Nazi atomic weapon development programme. Unfortunately, both gliders were forced to crash-land far from their objective and one tug crashed into mountains. Of the two parties of engineers, some were killed during the crash landings and the remainder executed by the Nazis.

The principal glider of US airborne forces was the Waco, known as the Hadrian when used by the British, which entered service in 1942. Constructed from tubular steel and wood with a fabric skin and wooden floor, it could carry fifteen fully equipped troops including the two crew. Normally towed by a C-47, it had a maximum towing speed of 125 mph (201 km/hr). The first major operational use of the Waco was in July 1943 during the invasion of Sicily in which 1st Airborne Division took part. Eight Horsa gliders and 144 Wacos/Hadrians flew 1st Airlanding Brigade and gliderborne elements of the division's two parachute brigades to landing zones on the east coast of the island. Unfortunately a combination of adverse weather, heavy anti-aircraft fire (some of it from Allied ships off the coast), and inexperienced tug pilots resulted in heavy losses within the division which nevertheless succeeded in taking its objectives.

The next major operation involving the use of gliders was the invasion of Normandy. On the night of 5/6 June a company group of 2nd Battalion Oxfordshire & Buckinghamshire Light Infantry, one of the battalions of 6th Airborne Division's 6th Airlanding Brigade, was landed in a successful coup de main operation on two bridges over the river Orne and Caen Canal. So accurate was the landing that the leading glider's nose was within feet of the location indicated to the pilot during the briefings. A further coup de main operation involving the use of gliders was carried out on the same night at Merville, on the Normandy coast, where a successful attack was carried out on an enemy gun battery.

Gliders featured largely in the main landings on 6 June of 6th Airborne Division and the 82nd and 101st US Airborne Divisions. Ninety-eight Horsas and Hamilcars brought in Headquarters 6th Airborne Division and support elements for 3rd and 5th Parachute Brigades, while a further 256 brought in 1st Airlanding Brigade and divisional troops in a subsequent lift. Meanwhile, 514 Wacos and Horsas were used to bring in the two glider infantry regiments and divisional troops of the two American divisions.

Two months later, gliders were used in BLUEBIRD and DOVE which formed part of DRAGOON, the landings in southern France in August 1944. Four hundred and three Wacos were used to transport airlanding elements of 1st Airborne Task Force. The landings were all successful, with 95 per cent of gliders reaching the landing zones successfully. Gliders were also employed extensively in MARKET GARDEN, the ill-fated Arnhem operation in Holland in September 1944. A total of 1, 295 were used to lift the airlanding and divisional troop elements of I Airborne Corps, comprising 1st Airborne Division and 82nd and 101st US Airborne Divisions. In March 1945 XVIII US Airborne Corps, comprising 6th Airborne Division and 17th US Airborne Division, led the assault during VARSITY, the crossing of the Rhine; 1, 348 Horsas, Hamilcars, and Wacos took part but suffered very heavy casualties from enemy ground fire as they landed under fire on flat, grassy terrain in full view of the enemy. The operation was nevertheless successful and all objectives were taken by the end of the first day.

Japan produced a number of gliders but none saw operational service. The best was the Ku-7 which, with a maximum payload of 16, 450 lb (7, 461.7 kg), could carry a light tank or 32 fully equipped troops and was towed by either a Nakajima Ki-49 or Mitsubishi Ki-67.

The first Soviet glider was the Antonov A-7 which appeared in 1939. Carrying eight men or 1 ton of cargo, it was used to supply partisan units. After the war, Soviet development of gliders continued with the YAK-14 which had a maximum towing speed of 180 mph (290 km/ph), a payload of 7, 700 lb (3, 492.7 kg), and could carry 35 troops. Two other gliders, the TS-25 and IL-32, capable of carrying 25 and 35 troops respectively, were also produced.

Gliders played an important role in airborne warfare during WW II, transporting large numbers of troops, heavy weapons, and equipment. They also proved useful in coup de main operations, having the advantages of silence and the capability of landing within very short distances. However, they were vulnerable to attack from both the air and ground and, as landings were frequently under heavy fire, the costs in aircrew and aircraft were very high. During the post-war period, the role of the glider was gradually assumed by the helicopter which saw increasing operational use from the 1950s onwards.

Bibliography

  • Chatterton, Brig. George, The Wings of Pegasus: The Story of The Glider Pilot Regiment (London, 1962).
  • Harclerode, Peter, Go to It! The History of The 6th Airborne Division (London, 1990).
  • Otway, Lt Col T. B. H., The Second World War 1939-1945: Army Airborne Forces (London, 1990).
  • Wood, Alan, History of The World's Glider Forces (London, 1992)

— Peter Harclerode

n. 1. a light aircraft that is designed to fly for long periods without using an engine.

2. the pilot of such an aircraft.

See the Introduction, Abbreviations and Pronunciation for further details.

The military glider, unique to World War II, became obsolete after the war as aviation developed, especially with the production of successful Helicopters.

The Germans conducted the first glider mission in 1940. Recognizing the possibilities, the British and Americans implemented their own glider programs designed to discharge, in a small area, large numbers of fully armed troops ready for immediate combat, thus eliminating the costly time required to assemble paratroopers. Gliders also made it possible to deliver vehicles and weapons too heavy for parachutes.

The Germans made the most imaginative use of gliders to land troops silently on top of the Belgian Fort Eben-Emael in May 1940. Within ten minutes they blinded that great fortress, virtually putting it out of action. In May 1941 the only large-scale employment of gliders by the Luftwaffe played a significant role in Operation Merkur, the successful airborne assault on Crete. A daring, small-scale glider mission liberated Benito Mussolini from imprisonment at Gran Sasso in the Abruzzi Mountains in Italy in 1943. Elsewhere, minor glider missions substituted when transport aircraft operations were not feasible.

Allied forces used gliders on a larger scale. The first operation, in 1943, a British-American assault on Sicily, provided valuable experience despite being inept and costly. Use of gliders on D day in Normandy was largely successful but indecisive. The largest Allied glider mission, part of Operation Market-Garden in September 1944, employed 2,596 gliders to secure a bridgehead across the Rhine River at Arnhem, Netherlands, but had limited success. Operation Varsity, the last glider operation of the war, near Wesel, Germany, on 23 March 1945, employed 1,348 gliders and was considered a tremendous success.

Bibliography

Craven, Wesley F., and James Lea Cate, eds. The Army Air Forces in World War II. Chicago: University of Chicago Press, 1950–1958.

U.S. Air Force. USAF Historical Studies, Air Force Historical Research Agency, nos. 1, 97, and 167.

—John A. McQuillen Jr./C. W.

glider, type of aircraft resembling an airplane but having at most a small auxiliary propulsion plant and usually no means of propulsion at all. The typical modern glider has very slender wings and a streamlined body. The unpowered variety is launched by an elastic shock cord, a rope, or a cable, attached to the front of the glider and pulled by a launching crew, a winch, a tow car, or a tow plane. Gliders can be towed behind airplanes over great distances. The powered variety can take off and climb on its own. The glider uses gravity and updrafts of air to keep it flying; slope soaring relies on wind rising off dunes or hillsides, while thermal soaring exploits convection currents in the air. In soaring the glider is repeatedly maneuvered through updrafts to reach altitudes as high as 46,000 ft (14,000 m). It can then glide down through air that is not rising. In a powered glider the engine can be turned on to keep the glider aloft when there are no updrafts. A sailplane, a glider which is built especially for soaring and sustained flight, can travel as much as 500 mi (800 km) in this manner. The usual flight controls in a glider consist of a pedal to operate the rudders and a control stick to operate the elevators and ailerons. Otto and Gustav Lilienthal of Germany made the first successful piloted glider flight in 1891. The Lilienthals demonstrated the superiority of curved over flat surfaces in flight and encouraged others to make glider experiments, at least until Otto's death in a glider crash in 1896. At the beginning of the 20th cent. the Wright brothers constructed and flew many gliders. They introduced land skids, wing warping, and other improvements that characterize present-day gliders. In World War II troop-transport gliders were used for aerial invasions. The gliders were launched and towed by cargo aircraft to the invasion area, where they were released. Early gliders were launched from hills or by running forward; the machine maintained stability while in flight by the pilot's shifting body weight. These techniques have been resurrected in modern hang gliding, a development based on NASA experiments with flexible-wing gliders in the 1950s. The hang glider, with nylon or Kevlar stretched over an aluminum frame, can reach an altitude of 20,000 ft (6,100 m) and stay aloft up to 15 hours; in 1979 five hang glider pilots flew their machines (fitted with auxiliary motors) across the United States. A paraglider is an parachutelike airfoil made of nylon and Mylar from which the pilot is suspended by a series of ropes. Paraglider pilots must "kite"-raise the airfoil into the air by running and using the wind-before launching themselves from a cliff or the like.

Bibliography

See T. L. Knauff, Glider Basics from First Flight to Solo (1982); D. Piggott, Gliding (5th ed. 1987).


A heavier-than-air aircraft supported in flight by the dynamic reaction of the air against its lifting surfaces and whose free flight does not depend principally on an engine. Gliders are designed to glide, or glide and soar. Gliders are launched by aircraft tows, automobiles, winches, or catapults. Once in the air, they soar in thermals and glide down slowly. High-performance gliders are known as sailplanes.

Gliding marsupials equipped with lateral membranes connecting the fore and hindlimbs; includes Petaurus breviceps (sugar glider), Petauroides volans (greater glider) and Acrobates pygmaeus (feather-tailed glider).

Random House Word Menu:

categories related to 'glider'

Top
Random House Word Menu by Stephen Glazier
For a list of words related to glider, see:
  • Marsupials
  • Types of Aircraft - glider: heavier-than-air craft supported in flight by action of air against lifting surfaces, not dependent on engine and usu. not having one; sailplane


Wikipedia on Answers.com:

Glider (sailplane)

Top
Glider
Single-seat high performance fiberglass Glaser-Dirks DG-808 over the Lac de Serre Ponçon in the French Alps
Part of a series on
Categories of aircraft
Supported by lighter-than-air gases (aerostats)
Unpowered Powered
Supported by LTA gases + aerodynamic lift
Unpowered Powered
Supported by aerodynamic lift (aerodynes)
Unpowered Powered
Unpowered fixed-wing Powered fixed-wing
Powered hybrid fixed/rotary wing
Unpowered rotary-wing Powered rotary-wing
Powered aircraft driven by flapping
Other means of lift
Unpowered Powered
Glider2010-overgunma.ogv
(video) A glider sails over Gunma, Japan.

A glider or sailplane is a type of glider aircraft used in the sport of gliding.[1][2] They have rigid wings and an undercarriage.[2] Some gliders, known as motor gliders are also used for gliding and soaring, but have engines which can be used for extending a flight and, for some types, for take-off. Aircraft such as hang gliders and paragliders are foot-launched and so are described in separate articles, though their differences from sailplanes are covered below. Glider aircraft that are used for purposes other than recreation, for example for military purposes, do not soar.

Sports gliders benefit from creating the least drag for any given amount of lift, and this is best achieved with long, thin wings and a fully faired narrow cockpit. Aircraft with these features are able to climb efficiently in rising air and can glide long distances at high speed with a minimum loss of height in between.

Contents

Use of engines

Although most gliders do not have engines, there are a few that do. (see Motor glider). The manufacturers of high-performance gliders will list an optional engine with a retractable propeller that can be used to sustain flight, if required; these are known as 'self-sustaining' gliders. Some have enough thrust to launch themselves before the engine is retracted and are known as 'self-launching' gliders. There are also 'touring motor gliders' which can self launch and switch off the engine in flight without retracting their propellers.[3]

History

HAWA Vampyr 1921

Sir George Cayley's gliders achieved brief wing-borne hops from around 1849.[4] Otto Lilienthal built (barely) controllable gliders in the 1890s using weight shift with which he could ridge soar. The Wright Brothers achieved full control in the early 1900s using movable surfaces, to which they successfully added an engine.

After World War I gliders were built for sporting purposes in Germany (see link to Rhön-Rossitten Gesellschaft) and in the United States (Schweizer brothers). Germany's strong links (continuing today) to gliding were to a large degree due to Post-WWI regulations forbidding the construction and flight of motorised planes in Germany, so the country's aircraft enthusiasts often turned to gliders[5] and were actively encouraged by the German government.[6]

The sporting use of gliders rapidly evolved in the 1930s and is now the main application. As their performance improved, gliders began to be used for cross-country flying and now regularly fly hundreds or even thousands of kilometers in a day[7][8] if the weather is suitable.

Glider design

Early gliders had no cockpit and the pilot sat on a small seat located just ahead of the wing. These were known as "primary gliders" and they were usually launched from the tops of hills, though they are also capable of short hops across the ground while being towed behind a vehicle. To enable gliders to soar more effectively than primary gliders, the designs minimized drag. Gliders now have very smooth, narrow fuselages and very long, narrow wings with a high aspect ratio and winglets.

Cockpit of a typical modern glider (Glaser-Dirks DG-101G ELAN).
Click on the image for an explanation of the instrumentation.
A glider releasing its water ballast

The early gliders were made mainly of wood with metal fastenings, stays and control cables. Later fuselages made of fabric-covered steel tube were married to wood and fabric wings for lightness and strength. New materials such as carbon-fiber, fiber glass and Kevlar have since been used with computer-aided design to increase performance. The first glider to use glass-fiber extensively was the Akaflieg Stuttgart FS-24 Phönix which first flew in 1957. This material is still used because of its high strength to weight ratio and its ability to give a smooth exterior finish to reduce drag. Drag has also been minimized by more aerodynamic shapes and retractable undercarriages. Flaps are fitted to the trailing edges of the wings on some gliders to minimise the drag from the tailplane at all speeds.

With each generation of materials and with the improvements in aerodynamics, the performance of gliders has increased. One measure of performance is the glide ratio. A ratio of 30:1 means that in smooth air a glider can travel forward 30 meters while losing only 1 meter of altitude. Comparing some typical gliders that might be found in the fleet of a gliding club - the Grunau Baby from the 1930s had a glide ratio of just 17:1, the glass-fiber Libelle of the 1960s increased that to 39:1, and modern flapped 18 meter gliders such as the ASG29 have a glide ratio of over 50:1. The largest open-class glider, the eta, has a span of 30.9 meters and has a glide ratio over 70:1. Compare this to the infamous Gimli Glider, a Boeing 767 which ran out of fuel mid-flight and was found to have a glide ratio of only 12:1, or to the Space Shuttle with a glide ratio of 4.5:1.[9]

Due to the critical role that aerodynamic efficiency plays in the performance of a glider, gliders often have aerodynamic features seldom found in other aircraft. The wings of a modern racing glider have a specially designed low-drag laminar flow airfoil. After the wings' surfaces have been shaped by a mold to great accuracy, they are then highly polished. Vertical winglets at the ends of the wings are computer-designed to decrease drag and improve handling performance. Special aerodynamic seals are used at the ailerons, rudder and elevator to prevent the flow of air through control surface gaps. Turbulator devices in the form of a zig-zag tape or multiple blow holes positioned in a span-wise line along the wing are used to trip laminar flow air into turbulent flow at a desired location on the wing. This flow control prevents the formation of laminar flow bubbles and ensures the absolute minimum drag. Bug-wipers may be installed to wipe the wings while in flight and remove insects that are disturbing the smooth flow of air over the wing.

Modern competition gliders carry jettisonable water ballast (in the wings and sometimes in the vertical stabilizer). The extra weight provided by the water ballast is advantageous if the lift is likely to be strong, and may also be used to adjust the glider's center of mass. Moving the center of mass toward the rear by carrying water in the vertical stabilizer reduces the required down-force from the horizontal stabilizer and the resultant drag from that down-force. Although heavier gliders have a slight disadvantage when climbing in rising air, they achieve a higher speed at any given glide angle. This is an advantage in strong conditions when the gliders spend only little time climbing in thermals. The pilot can jettison the water ballast before it becomes a disadvantage in weaker thermal conditions. Another use of water ballast is to dampen air turbulence such as might be encountered during ridge soaring. To avoid undue stress on the airframe, gliders must jettison any water ballast before landing.

Most gliders are built in Europe and are designed to EASA Certification Specification CS-22 (previously Joint Aviation Requirements-22). These define minimum standards for safety in a wide range of characteristics such as controllability and strength. For example, gliders must have design features to minimize the possibility of incorrect assembly (gliders are often stowed in disassembled configuration, with at least the wings being detached). Automatic connection of the controls during rigging is the common method of achieving this.

Launch and flight

Double aerotow

The two most common methods of launching sailplanes are by aerotow and by winch.[10] When aerotowed, the glider is towed behind a powered aircraft using a rope about 60 meters (about 200 ft) long. The glider pilot releases the rope after reaching the desired altitude. However, the rope can be released by the towplane also. Winch launching uses a powerful stationary engine located on the ground at the far end of the launch area. The glider is attached to one end of 800–1200 metres (about 2,500-4,000 ft) of cable and the winch rapidly winds it in. The glider can gain about 1200–2000 feet of height with a winch launch (about 400 – 600 metres), depending on the head wind. Less often, automobiles are used to pull gliders into the air, by pulling them directly or through the use of a reverse pulley in a similar manner to the winch launch. Elastic ropes (known as bungees) are occasionally used at some sites to launch gliders from slopes, if there is sufficient wind blowing up the hill. Bungee launching was the predominant method of launching early gliders. Some modern sailplanes can self-launch with the use of retractable engines and/or propellers, which can also be used to sustain flight once airborne (see motor glider).

Once launched sailplanes try to gain height using thermals, ridge lift or lee waves and can remain airborne for hours. This is known as 'soaring'. By finding lift sufficiently often experienced pilots fly cross-country, often on pre-declared tasks of hundreds of kilometers, usually back to the original launch site. Cross-country flying and aerobatics are the two forms of competitive gliding. For information about the forces in gliding flight, see lift-to-drag ratio.

Glide slope control

Pilots need some form of control over the glide slope to land the glider. In powered aircraft, this is done by reducing engine thrust. In gliders, other methods are used to either reduce the lift generated by the wing, increase the drag of the entire glider, or both. Glide slope is the distance traveled for each unit of height lost. In a steady wings-level glide with no wind, glide slope is the same as the lift/drag ratio (L/D) of the glider, called "L-over-D". Reducing lift from the wings and/or increasing drag will reduce the L/D allowing the glider to descend at a steeper angle with no increase in airspeed. Simply pointing the nose downwards only converts altitude into a higher airspeed with a minimal initial reduction in total energy. Gliders, because of their long low wings, create a high ground effect which can significantly increase the glide angle and make it difficult bring the glider to Earth in a short distance.

  • Sideslipping - A slip is performed by crossing the controls (rudder to right with ailerons to left, for example) so that the glider is no longer flying aligned with the air flow. This will present one side of the fuselage to the air-flow significantly increased drag. Early gliders primarily used slipping for glide slope control.
  • Spoilers - Spoilers are movable control surfaces in the top of the wing, usually located mid-chord or near the spar which are raised into the air-flow to eliminate (spoil) the lift from the wing area behind the spoiler, disrupting the spanwise distribution of lift and increasing lift-induced drag. Spoilers significantly increase drag.
  • Air brakes - Air brakes, also known as dive brakes, are devices whose primary purpose is to increase drag. On gliders, the spoilers act as air brakes. They are positioned on top of the wing and below the wing also. When slightly opened the upper brakes will spoil the lift, but when fully opened will present a large surface and so can provide significant drag. Some gliders have terminal velocity dive brakes, which provide enough drag to keep its speed below maximum permitted speed, even if the glider were pointing straight down. This capability is considered a safer way to descend without instruments through cloud (or to descend vertically in confined terrain), than the only alternative, an intentional spin.
  • Flaps - Flaps are movable surfaces on the trailing edge of the wing. The primary purpose of flaps is to change the camber of the wing and so change the lift-to-drag ratio of the wing. This reduces the stall speed and so allows reduced landing speeds. It was possible to lower the flaps on some older gliders by up to 90 degrees to increase drag significantly as well as increasing lift coefficient when landing. Another feature that flapped gliders possess are negative flaps that are also able to deflect the trailing edge upward. This feature is included on some competition sailplanes in order to reduce the pitching moment on the wing and allowing better glide ratios at higher speeds (a particularly desirable characteristic for racing sailplanes).
  • Parachute - Some high performance gliders from the 1960s and 1970s were designed to carry a small drogue parachute because their air brakes are not particularly effective. This is stored in the tail-cone of the glider during flight. When deployed, a parachute causes a large increase in drag, but has a significant disadvantage over the other methods of controlling the glide slope. This is because a parachute does not allow the pilot to finely adjust the glide slope. Consequently a pilot may have to jettison the parachute entirely, if the glider is not going to reach the desired landing area.

Landing

A typical training glider, Schleicher ASK 21 just before landing

Early glider designs used skids for landing, but modern types generally land on wheels. Some of the earliest gliders used a dolly with wheels for taking off and the dolly was jettisoned as the glider left the ground, leaving just the skid for landing. A glider may be designed so the center of gravity (CG) is behind the main wheel so the glider sits nose high on the ground. Other designs may have the CG forward of the main wheel so the nose rests on a nose-wheel or skid when stopped. Skids are now mainly used only on training gliders such as the Schweizer SGS 2-33. Skids are around 100mm (3 inches) wide by 900mm (3 feet) long and run from the nose to the main wheel. Skids help with braking after landing by allowing the pilot to put forward pressure on the control stick, thus creating friction between the skid and the ground. The wing tips also have small skids or wheels to protect the wing tips from ground contact.

In most high performance gliders the undercarriage can be raised to reduce drag in flight and lowered for landing. Wheel brakes are provided to allow stopping once on the ground. These may be engaged by fully extending the spoilers/air-brakes or by using a separate control. Although there is only a single main wheel, the glider's wing can be kept level by using the flight controls until it is almost stationary.

Pilots usually land back at the airfield from which they took off, but a landing is possible in any flat field about 250 metres long. Ideally, should circumstances permit, a glider would fly a standard pattern, or circuit, in preparation for landing, typically starting at a height of 300 metres (1,000 feet). Glide slope control devices are then used to adjust the height to assure landing at the desired point. The ideal landing pattern positions the glider on final approach so that a deployment of 30-60% of the spoilers/dive brakes/flaps brings it to the desired touchdown point. In this way the pilot has the option of opening or closing the spoilers/air-brakes to extend or steepen the descent to reach the touchdown point. This gives the pilot wide safety margins should unexpected events occur.

Instrumentation and other technical aids

Schempp-Hirth Janus-C in flight, showing instrument panel configured in the basic-T, with airspeed, turn and bank and altitude displays across the top row; below a GPS-driven computer, with wind and glide information, drives two electronic variometer displays to the right. The yaw string and compass are above the glare shield

In addition to an altimeter, compass, and an airspeed indicator, gliders are often equipped with a variometer, turn and bank indicator and an airband radio (transceiver), each of which may be required in some countries. An Emergency Position-Indicating Radio Beacon (ELT) may also be fitted into the glider to reduce search and rescue time in case of an accident.

Much more than in other types of aviation, glider pilots depend on the variometer, which is a very sensitive vertical speed indicator, to measure the climb or sink rate of the plane. This enables the pilot to detect minute changes caused when the glider enters rising or sinking air masses. Both mechanical and electronic 'varios' are usually fitted to a glider. The electronic variometers produce a modulated sound of varying amplitude and frequency depending on the strength of the lift or sink, so that the pilot can concentrate on centering a thermal, watching for other traffic, on navigation, and weather conditions. Rising air is announced to the pilot as a rising tone, with increasing pitch as the lift increases. Conversely, descending air is announced with a lowering tone, which advises the pilot to escape the sink area as soon as possible. (Refer to the variometer article for more information).

Gliders' variometers are sometimes fitted with mechanical devices such as a "MacCready Ring" to indicate the optimal speed to fly for given conditions. These devices are based on the mathematical theory attributed to Paul MacCready[11] though it was first described by Wolfgang Späte in 1938.[12] MacCready theory solves the problem of how fast a pilot should cruise between thermals, given both the average lift the pilot expects in the next thermal climb, as well as the amount of lift or sink he encounters in cruise mode. Electronic variometers make the same calculations automatically, after allowing for factors such as the glider's theoretical performance, water ballast, headwinds/tailwinds and insects on the leading edges of the wings.

Soaring flight computers, often used in combination with PDAs running specialized soaring software, have been designed for use in gliders. Using GPS technology in conjunction with a barometric device these tools can:

  • Provide the glider's position in 3 dimensions by a moving map display
  • Alert the pilot to nearby airspace restrictions
  • Indicate position along track and remaining distance and course direction
  • Show airports within theoretical gliding distance
  • Determine wind direction and speed at current altitude
  • Show historical lift information
  • Create a GPS log of the flight to provide proof for contests and gliding badges
  • Provide "final" glide information (i.e. showing if the glider can reach the finish without additional lift).
  • Indicate the best speed to fly under current conditions

After the flight the GPS data may be replayed on computer software for analysis and to follow the trace of one or more gliders against a backdrop of a map, an aerial photograph or the airspace.

Because collision with other gliders is a risk, the anti-collision device FLARM is becoming increasingly common in Europe and Australia. In the longer term, gliders may eventually be required in some European countries to fit transponders once devices with low power requirements become available.

Swift S-1 of the UK Swift Aerobatic Display Team at Kemble 2009

Markings

To distinguish gliders in flight, very large numbers/letters are sometimes displayed on the fin and wings. Registrations on narrow fuselages are difficult to read. These numbers were first added for use by ground-based observers in competitions, and are therefore known as "competition numbers" or "contest IDs".[13] They are unrelated to the glider's registration number, and are assigned by national gliding associations. They are useful in radio communications between gliders, so glider pilots often use their competition number as their call signs.

Fibreglass gliders are white in color after manufacture. Since fibreglass resin softens at high temperatures, white is used almost universally to reduce temperature rise due to solar heating. Color is not used except for a few small bright patches on the wing tips; these patches (typically bright red) improve gliders' visibility to other aircraft while in flight (and are a requirement for mountain flying in France).[14] Non-fibreglass gliders (those made of aluminum and wood) are not subject to the temperature-weakening problem of fibreglass, and can be painted any color at the owner's choosing; they are often quite brightly painted.

Comparison of gliders with hang gliders and paragliders

There is sometimes confusion about gliders, hang gliders and paragliders. In particular paragliders and hang gliders are both foot-launched. The main differences between the types are:

Paragliders Hang gliders Gliders/Sailplanes
Undercarriage Pilot's legs used for take-off and landing Pilot's legs used for take-off and landing Aircraft takes off and lands using a wheeled undercarriage or skids
Wing structure entirely flexible, with shape maintained purely by the pressure of air flowing into and over the wing in flight and the tension of the lines generally flexible but supported on a rigid frame which determines its shape, but note that rigid wing hang gliders also exist rigid surface to wings that totally encases structure
Pilot position sitting supine in a seated harness. usually lying prone in a cocoon-like harness suspended from the wing. Seated, and 'supine' are also possible. sitting in a seat with a harness surrounded by a crash-resistant structure.
Speed range
(stall speed – max speed)
slower – typically 25 to 60km/h for recreational gliders (over 40km/h requires use of speed bar)[15] hence easier to launch and fly in light winds, least wind penetration, pitch variation can be achieved with the controls. easier to launch and fly in stronger conditions with better wind penetration[citation needed] even faster - maximum speed up to about 280 km/h (170 mph); stall speed typically 65 km/h (40mph). Able to fly in windier turbulent conditions and can outrun bad weather. Exceptional penetration into the wind. Semi- or fully aerobatic.
Maximum glide ratio about 10, relatively poor glide performance makes long-distances more difficult. The current world record is just above 500 km (310 miles)[16] Open class sailplanes typically around 60:1 but in more common 15-18 meter span aircraft, glide ratios are between 38:1 and 52:1. [17], high glide performance enabling long distances, 3,000 km (1,800+ mile record)[18]
Turn radius tighter turn radius, allowing circling in the rapidly rising center of thermals[citation needed] somewhat larger turn radius, not allowing such a high rate of climb in thermals[citation needed] even greater turn radius but still able to circle tightly in thermals[19]
Landing smaller space needed to land, offering more landing options from cross-country flights. Also easier to carry back to the nearest road longer approach & landing area required, but can reach more landing areas due superior glide range Specialised trailer needed to retrieve by road
Learning simplest and quickest to learn teaching is done in a two seat glider with dual controls
Convenience packs smaller (easier to transport and store); lighter (can be easily carried considerable distances); quicker to rig & de-rig; transported in the trunk of a car[citation needed] more awkward to transport & store; longer to rig and de-rig; transported on the roof of a car trailers are typically 10 m (30 ft) long. Rigging & de-rigging takes about 20 minutes
Cost cost new €2000 up[20], cheapest but shortest lasting (around 500 hours flying depending on treatment) but active second hand market[21] cost of new gliders very high but long lasting (several decades), so active second hand market typically from €2000 to €145,000[22] .

Competition classes of glider

DG Flugzeugbau DG-1000 of the Two Seater Class

Eight competition classes of glider have been defined by the FAI.[23] They are:

  • Standard Class (No flaps, 15 m wing-span, water ballast allowed)
  • 15 metre Class (Flaps allowed, 15 m wing-span, water ballast allowed)
  • 18 metre Class (Flaps allowed, 18 m wing-span, water ballast allowed)
  • Open Class (No restrictions except a limit of 850 kg for the maximum all-up weight)
  • Two Seater Class (maximum wing-span of 20 m), also known by the German name "Doppelsitzer"
  • Club Class (This class allows a wide range of older small gliders with different performance and so the scores have to be adjusted by handicapping. Water ballast is not allowed).
  • World Class (The FAI Gliding Commission which is part of the FAI and an associated body called Organisation Scientifique et Technique du Vol à Voile (OSTIV) announced a competition in 1989 for a low-cost glider, which had moderate performance, was easy to assemble and to handle, and was safe for low hours pilots to fly. The winning design was announced in 1993 as the Warsaw Polytechnic PW-5. This allows competitions to be run with only one type of glider.
  • Ultralight Class, for gliders with a maximum mass less than 220 kg.

Major manufacturers of gliders

A large proportion of gliders have been and are still made in Germany [24] the birthplace of the sport. The principal German manufacturers are:

though there are other specialist manufacturers in Germany, Poland and in other eastern European countries.[25]

See also

Gliding as a sport
Other unpowered aircraft
Unpowered flying toys and models

References

  1. ^ FAA Glider handbook
  2. ^ a b Definition of gliders used for sporting purposes in FAI Sporting Code
  3. ^ Civil Aviation Authority; Civil Aviation Authority: Personnel Licensing Department - Flight Crew (2005-12-02). LASORS 2006: The Guide for Pilots. The Stationery Office. ISBN 978-0-11-790501-6. http://books.google.com/?id=_z6d-q_X4MAC. 
  4. ^ Flight magazine 1954
  5. ^ "History of Gliding & Soaring". United States Soaring Team. Updated 7 August 2004. http://www.ssa.org/test/UsTeam/adobe%20pdf/pr%20pdf/BR%20Soaring%20History%20V5%2004.pdf. Retrieved 23 February 2010. 
  6. ^ Gliding Magazine | Features
  7. ^ List of FAI ratified world records[dead link]
  8. ^ On-line contest web page
  9. ^ Space Shuttle Technical Conference pg 258
  10. ^ Piggott, Derek (2002-03-01). Gliding: A handbook on soaring flight. A & C Black. ISBN 978-0-7136-6148-4. http://books.google.com/?id=RsJzPwAACAAJ. 
  11. ^ "MacCready Theory". Archived from the original on 2007-09-17. http://web.archive.org/web/20070917213823/http://home.att.net/~jdburch/polar.htm. Retrieved 2006-08-24. 
  12. ^ Pettersson, Åke (Oct-Nov 2006). "Letters". Sailplane & Gliding (British Gliding Association) 57 (5): 6. 
  13. ^ Reference to competition numbers on FAI web site[dead link]
  14. ^ Gliding In France
  15. ^ Technical data for Advance Omega 8 - accessed 22-10-2011
  16. ^ FAI Paragliding record - accessed 2010-11-30
  17. ^ Handicap list 2008 of the Deutscher Aero Club - accessed 2008-08-07
  18. ^ FAI records Accessed 30 November 2010
  19. ^ Stewart, Ken (1994). The Glider Pilot's Manual. Airlife Publishing Ltd. p. 257. ISBN 185310504X. 
  20. ^ major manufactures price list - accessed 2011-10-21
  21. ^ Typical set of classified ads
  22. ^ Typical set of classified ads
  23. ^ Competition classes as defined by FAI
  24. ^ Francis Humblet (Nov/Dec 2011). "World Glider Production". Gliding International. 
  25. ^ Simons, Martin (2002). Sailplanes 1965-2000. Eqip. ISBN 978-3-9808838-1-8. http://books.google.com/?id=9szZAAAAMAAJ. 

External links


Translations:

Glider

Top

Dansk (Danish)
n. - svævefly, svæveplan, glideplan, hængesofa

Nederlands (Dutch)
zweefvliegtuig, zweefvlieger, glijder, soort Australisch buideldier

Français (French)
n. - (Aviat) planeur, (US) balancelle double

Deutsch (German)
n. - Segelflugzeug, Segler

Ελληνική (Greek)
n. - ανεμόπτερο, ανεμοπλάνο

Italiano (Italian)
aliante

Português (Portuguese)
n. - planador (m), balanço (m) de varanda (Arquit.)

Русский (Russian)
планер, планерист

Español (Spanish)
n. - planeador, avión sin motor, velero

Svenska (Swedish)
n. - segelflygplan, segelflygare

中文(简体)(Chinese (Simplified))
滑行者, 吊椅, 滑翔机

中文(繁體)(Chinese (Traditional))
n. - 滑行者, 吊椅, 滑翔機

한국어 (Korean)
n. - 글라이더(활공기), 미끄러지는 것[사람]

日本語 (Japanese)
n. - グライダー, 滑空機, 滑るもの, ぶらんこいす

العربيه (Arabic)
‏(الاسم) طائرة شراعيه‏

עברית (Hebrew)
n. - ‮דאון, דואה, גלשן, גולש‬


Best of the Web:

glider

Top

Some good "glider" pages on the web:


How?
travel.howstuffworks.com
 
 
 

 

Copyrights:

American Heritage Dictionary. The American Heritage® Dictionary of the English Language, Fourth Edition Copyright © 2007, 2000 by Houghton Mifflin Company. Updated in 2009. Published by Houghton Mifflin Company. All rights reserved.  Read more
Britannica Concise Encyclopedia. Britannica Concise Encyclopedia. © 1994-2012 Encyclopædia Britannica, Inc. All rights reserved.  Read more
McGraw-Hill Science & Technology Encyclopedia. McGraw-Hill Encyclopedia of Science and Technology. Copyright © 2005 by The McGraw-Hill Companies, Inc. All rights reserved.  Read more
Oxford Companion to Military History. The Oxford Companion to Military History. Copyright © 2001, 2004 by Oxford University Press. All rights reserved.  Read more
Oxford Dictionary of the US Military. The Oxford Essential Dictionary of the U.S. Military. Copyright © 2001, 2002 by Oxford University Press, Inc. All rights reserved.  Read more
$copyright.smallImage.alttext Gale Encyclopedia of US History. Encyclopedia of American History Copyright © 2006 by The Gale Group, Inc. All rights reserved.  Read more
Columbia Encyclopedia. The Columbia Electronic Encyclopedia, Sixth Edition Copyright © 2012, Columbia University Press. Licensed from Columbia University Press. All rights reserved. www.cc.columbia.edu/cu/cup/ Read more
McGraw-Hill Dictionary of Aviation. An Illustrated Dictionary of Aviation.. Copyright © 2005 by McGraw-Hill Companies, Inc. All rights reserved.  Read more
Saunders Veterinary Dictionary. Saunders Comprehensive Veterinary Dictionary 3rd Edition. Copyright © 2007 by D.C. Blood, V.P. Studdert and C.C. Gay, Elsevier. All rights reserved.  Read more
Random House Word Menu. © 2010 Write Brothers Inc. Word Menu is a registered trademark of the Estate of Stephen Glazier. Write Brothers Inc. All rights reserved.  Read more
 Rhymes. Oxford University Press. © 2006, 2007 All rights reserved.  Read more
Wikipedia on Answers.com. This article is licensed under the Creative Commons Attribution/Share-Alike License. It uses material from the Wikipedia article Glider (sailplane) Read more
Translations. Copyright © 2007, WizCom Technologies Ltd. All rights reserved.  Read more

Follow us
Facebook Twitter
YouTube

Mentioned in

» More» More

Related topics