Glider (sailplane)

Source: Wikipedia, the free encyclopedia.

Rolladen-Schneider LS4
(video) A glider sails over
Gunma
, Japan.

A glider or sailplane is a type of

glider aircraft used in the leisure activity and sport of gliding (also called soaring).[1][2] This unpowered aircraft
can use naturally occurring currents of rising air in the atmosphere to gain altitude. Sailplanes are aerodynamically streamlined and so can fly a significant distance forward for a small decrease in altitude.

In North America the term 'sailplane' is also used to describe this type of aircraft. In other parts of the English-speaking world, the word 'glider' is more common.

Types

ASH25M—a self-launching two-seater glider

Gliders benefit from producing very low

long, thin wings, a slender fuselage
and smooth surfaces with an absence of protuberances. Aircraft with these features are able to soar – climb efficiently in rising air produced by thermals or hills. In still air, sailplanes can glide long distances at high speed with a minimum loss of height in between.

Sailplanes have rigid wings and either skids or undercarriage.[2] In contrast hang gliders and paragliders use the pilot's feet for the start of the launch and for the landing. These latter types are described in separate articles, though their differences from sailplanes are covered below. Sailplanes are usually launched by winch or aerotow, though other methods, auto tow and bungee, are occasionally used.

These days almost all gliders are sailplanes, but in the past many gliders were not. These types did not soar. They were simply engine-less aircraft towed by another aircraft to a desired destination and then cast off for landing. The prime example of non-soaring gliders were military gliders (such as those used in the Second World War). They were often used just once and then usually abandoned after landing, having served their purpose.

Motor gliders are gliders with engines which can be used for extending a flight and even, in some cases, for take-off. Some high-performance motor gliders (known as "self-sustaining" gliders) may have an engine-driven retractable propeller which can be used to sustain flight. Other motor gliders have enough thrust to launch themselves before the engine is retracted and are known as "self-launching" gliders. Another type is the self-launching "touring motor glider", where the pilot can switch the engine on and off in flight without retracting the propeller.[3]

History

Hannover H 1 Vampyr, 1921

Wright Brothers
built gliders using movable surfaces for control. In 1903, they successfully added an engine.

After World War I gliders were first built for sporting purposes in Germany. Germany's strong links to gliding were to a large degree due to post-World War I 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, particularly at flying sites suited to gliding flight like the Wasserkuppe.[6]

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

Design

Early gliders had no

winglets
.

De-rigged glider in its trailer for storage and road transport

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

Flaps
are fitted to the trailing edges of the wings on some gliders to optimise lift and drag at a wide range of speeds.

With each generation of materials and with the improvements in

Eta, has a span of 30.9 meters and has a glide ratio over 70:1. Compare this to the Gimli Glider, a Boeing 767 which ran out of fuel mid-flight and was found to have a glide ratio of 12:1, or to the Space Shuttle with a glide ratio of 4.5:1.[9]

Left wing spar being inserted during rigging

High aerodynamic efficiency is essential to achieve a good gliding performance, and so gliders often have aerodynamic features seldom found in other aircraft. The wings of a modern racing glider are designed by computers to create a low-drag

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

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
ASK 13
Glider winch

The two most common methods of launching sailplanes are by aerotow and by winch.[10] When aerotowed, the sailplane is towed behind a powered aircraft using a rope about 60 metres (200 ft) long. The sailplane pilot releases the rope after reaching the desired altitude. However, the rope can be released by the towplane also in case of emergency. Winch launching uses a powerful stationary engine located on the ground at the far end of the launch area. The sailplane is attached to one end of 800 to 1,200 metres (2,600 to 3,900 ft) of cable and the winch rapidly winds it in. The sailplane can gain about 270 to 910 metres (900 to 3,000 ft) of height with a winch launch, depending on the headwind. Less often, automobiles are used to pull sailplanes into the air, either 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 gliders can self-launch by using retractable engines or just retractable propellers. (see motor glider). These engines can use internal combustion or battery power.[11]

Once launched, gliders try to gain height using

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 to 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 increasing 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
spin
.
Flaps
stall speed. Another feature that some flapped gliders possess is negative flaps that are also able to deflect the trailing edge upward a small amount. This feature is included on some competition gliders in order to reduce the pitching moment
acting on the wing and so reduce the downwards force that must be provided by the horizontal stabiliser; this reduces the induced drag acting on the stabilizer. On some types the flaps and ailerons are linked, known a 'flaperons'. Simultaneous movement of these allows a greater rate of roll.
Parachute
Some high performance gliders from the 1960s and 1970s were designed to carry a small drogue parachute because their air brakes were not particularly effective. This was 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

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

Schweizer SGS 2–33
. Skids are around 100 millimetres (4 in) wide by 900 mm (3 ft) 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

forward slip
to further steepen the glider slope.

Auxiliary engines

Most gliders require assistance to launch, though some have an engine powerful enough to launch unaided. In addition, a high proportion of new gliders have an engine which will sustain the glider in the air, but is insufficiently powerful to launch the glider. Compared with self-launchers these lower powered engines have advantages in weight, lower costs and pilot licensing. The engines can be electric, jet, or two-stroke gasoline.

  • Glider showing propeller of front electric sustainer.
    Glider showing propeller of front electric sustainer.
  • Small retractable jet engines are on some types such as this HPH Shark
    Small retractable jet engines are on some types such as this HPH Shark
  • Retractable turbo two-stroke sustainer engine
    Retractable turbo two-stroke sustainer engine
  • Turbo engine retracting 1
    Turbo engine retracting 1
  • Turbo engine retracting 2
    Turbo engine retracting 2
  • Turbo engine retracting 3
    Turbo engine retracting 3

Instrumentation and other technical aids

Instrument panel for a sailplane. Click on image to see a detailed description (Schempp-Hirth Ventus-3)

Gliders in continental Europe use metric units, like

m/s for lift and sink rate. In the United States, United Kingdom, Australia and some other countries gliders use knots and ft/min
in common with commercial aviation worldwide.

In addition to an

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

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. Most often electronic 'varios' are fitted to a glider, though mechanical varios are often installed as back-up. 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).

Variometers are sometimes fitted with mechanical or electronic devices to indicate the optimal

glider's theoretical performance
, water ballast, headwinds/tailwinds and insects on the leading edges of the wings.

Soaring flight computers 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.

Kemble
2009

Markings

So that ground-based observers may identify gliders in flight or in gliding competition, registration marks ("insignias" or "competition numbers" or "contest ID") are displayed in large characters on the underside of a single wing, and also on the fin and rudder. Registration marks are assigned by gliding associations such as the US Soaring Society of America, and are unrelated to national registrations issued by entities such as the US Federal Aviation Administration.[14] This need for visual ID has somewhat been supplanted by GPS position recording. Insignias are useful in two ways: First, they are used in radio communications between gliders, as pilots use their competition number as their call signs. Secondly, to easily tell a glider's contest ID when flying in close proximity to one another to alert them of potential dangers. For example, during gatherings of multiple gliders within thermals (known as "gaggles"), one pilot might report "Six-Seven-Romeo I am right below you".

Fibreglass gliders are invariably painted white to minimise their skin temperature in sunlight. Fibreglass resin loses strength as its temperature rises into the range achievable in direct sun on a hot day. Color is not used except for a few small bright patches on wing tips; these patches (typically orange or red) improving a glider's visibility to other airborne aircraft. Such patches are obligatory for mountain flying in France.[15]
Non-fibreglass gliders made of aluminum or wood are not so subject to deterioration at higher temperatures and are often quite brightly painted.

Comparison of types

There is sometimes confusion about gliders/sailplanes, 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 (note that rigid-wing hang gliders also exist) rigid wing surface which totally encases wing structure
Pilot position sitting in a 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)
slowest – typically 25 to 60 km/h for recreational gliders (over 50 km/h requires use of speed bar),[16] hence easier to launch and fly in light winds; least wind penetration; pitch variation can be achieved with the controls faster than paragliders, slower than gliders/sailplaines maximum speed up to about 280 km/h (170 mph);[17] stall speed typically 65 km/h (40 mph);[17] able to fly in windier turbulent conditions and can outrun bad weather; good penetration into a headwind
Maximum glide ratio about 10, relatively poor glide performance makes long distance flights more difficult; current (as of May 2017) world record is 564 kilometres (350 mi)[18] about 17, with up to 20 for rigid wings 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;[19] high glide performance enabling long distance flight, with 3,000 kilometres (1,900 mi) being current (as of November 2010) record[20]
Turn radius tightest turn radius[citation needed] somewhat larger turn radius than paragliders, tigher than gliders/sailplanes[citation needed] widest turn radius but still able to circle tightly in thermals[21]
Landing smallest space needed to land, offering more landing options from cross-country flights; also easiest to pack up and carry like a bag to the nearest road 15 m to 60 m length flat area required; can be derigged by one person and carried to the nearest road landings can be performed in ~250 m length field. Aerial retrieve may be possible but if not, specialized trailer needed to retrieve by road. Some sailplanes have engines that remove the need for an out-landing, if successfully started on time
Learning simplest and quickest to learn teaching is done in single and two-seat hang gliders teaching is done in a two-seat glider with dual controls
Convenience packs smaller (easier to transport and store) more awkward to transport and store; longer to rig and de-rig; often transported on the roof of a car often stored and transported in purpose-built trailers about 9 metres long, from which they are rigged. Although rigging aids allow a single person to rig a glider, usually the rigging involves 2 or 3 people. Some frequently used sailplanes are stored already rigged in hangars.
Cost cost of new is €1500 and up,[22] cheapest but shortest lasting (around 500 hours flying time, depending on treatment), active second-hand market[23] cost of new glider very high (top of the range 18 m turbo with instruments and trailer €200,000) but it is long lasting (up to several decades), so active second-hand market; typical cost is from €2,000 to €145,000[24]

Competition classes

DG Flugzeugbau DG-1000 of the Two Seater Class

Eight competition classes of glider have been defined by the FAI.[25] 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, so the scores have to be adjusted by handicapping. Water ballast is not allowed).
  • World Class (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

A large proportion of gliders have been and are still made in Germany,[26] the birthplace of the sport. In Germany there are several manufacturers but the three principal companies are:

Germany also has

Let Kunovice and HpH in the Czech Republic and AMS Flight in Slovenia.[27]

See also

History
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. .
  4. ^ Flight magazine 1954
  5. ^ "History of Gliding & Soaring" (PDF). United States Soaring Team. 7 August 2004. Archived from the original (PDF) on 6 June 2011. Retrieved 23 February 2010.
  6. ^ "Gliding Magazine | Features". Archived from the original on 26 July 2011. Retrieved 23 February 2010.
  7. ^ "List of FAI claimed and ratified records". Archived from the original on 16 March 2015. Retrieved 11 September 2014.
  8. ^ On-line contest web page
  9. ^ Space Shuttle Technical Conference pg 258
  10. .
  11. ^ "SFPE Europe Digital Issue 30". www.sfpe.org. Retrieved 13 July 2023.
  12. ^ "MacCready Theory". Archived from the original on 17 September 2007. Retrieved 24 August 2006.
  13. ^ Pettersson, Åke (October–November 2006). "Letters". Sailplane & Gliding. 57 (5). British Gliding Association: 6.
  14. ^ Reference to competition numbers on FAI web site Archived 7 October 2008 at the Wayback Machine
  15. ^ Gliding In France
  16. ^ "Technical data for Advance Omega 8". Advance AG. Archived from the original on 30 May 2013. Retrieved 22 October 2011.
  17. ^ a b Flight Manual of Scheicher ASW27b. Alexander Schleicher GmbH & Co. 2003.
  18. ^ "FAI Paragliding record". Fédération Aéronautique Internationale. Archived from the original on 9 May 2011. Retrieved 30 November 2010.
  19. ^ "Handicap list 2008" (PDF). Deutsche Meisterschaft im Streckensegelflug. Deutscher Aero Club. Archived from the original (PDF) on 24 February 2009. Retrieved 7 August 2008.
  20. ^ "FAI records". Fédération Aéronautique Internationale. Archived from the original on 11 September 2011. Retrieved 30 November 2010.
  21. .
  22. ^ "Brochures Ozone". Ozone France. Archived from the original on 27 October 2013. Retrieved 21 October 2011.
  23. ^ "Typical set of classified ads for paragliders". Archived from the original on 30 March 2012. Retrieved 22 October 2011.
  24. ^ "Typical set of classified ads for gliders". Archived from the original on 6 December 2010. Retrieved 18 January 2011.
  25. ^ Competition classes as defined by FAI
  26. ^ Francis Humblet (November–December 2011). "World Glider Production". Gliding International.
  27. .

External links

Information about all types of glider
FAI webpages