Formation flying is the flight of multiple objects in coordination. Formation flying occurs in nature among flying and gliding animals, and is also conducted in human aviation, often in military aviation and air shows.
A multitude of studies have been performed on the performance benefits of aircraft flying in formation. [1]
Birds have been known to receive performance benefits from formation flight for over a century, through aerodynamic theory of Wieselsberger in 1914. [1] [2]
Formation flight in human aviation originated in World War I, when fighter aircraft were assigned to escort reconnaissance aircraft. [3] It was found that pairs of aircraft were more combat effective than single aircraft, and therefore, military aircraft would always fly in formations of at least two. [3] By World War II, pilots had discovered other strategic advantages to formation flight such as enhanced stability and optimal visibility.[ citation needed ]
It is a common misunderstanding to relate the reduction of drag in organized flight to the reduction of drag in drafting. However, they are quite different mechanistically.
The drag reduction occurred in the drafting is due to a reduction in flow speed in the wake of a leading vehicle, reducing the amount the flow needs to accelerate to move around the body, reducing pressure in front of the trailing vehicle. This leads to a lesser pressure differential between the frontal and rear projected surfaces of the body, and hence, less drag. This can also be understood somewhat tautologically through the common drag equation for a body , where is the experimentally obtained unitless number, is the density of the fluid medium through which the object travels, is the cross-sectional area normal to the direction mean flow, and is the speed of the mean flow. It can be seen by inspection, that a decrease in mean velocity will generate less drag force, as is the case with drafting.[ citation needed ]
In juxtaposition, the drag reduction felt by trailing agents in formation flight may be thought more of as the trailing agents "surfing" on the vortices shed by wings of leading agents, [4] reducing the amount of force needed to stay in the air. This force is known as lift and acts perpendicular to the freestream flow direction and drag. These vortices are known as wingtip vortices and are formed by fluid flowing around the wingtips from the high-pressure region that is the bottom of the wing to the low-pressure region that is the top of the wing. The flow becomes separated from the airfoil and rotates about a low pressure wake that forms the core of the vortex. This vortex acts to change the direction of the flow for trailing aircraft, increasing the lift over a segment of the wing and allowing for a reduction in induced drag by lowering its angle of attack. [5]
This can also be shown by the drag and analogous lift equation, . The difference now is that and vary linearly with angle of attack , which is the angle formed by the neutral axis of the aircraft and the freestream flow. Since the local flow is coming in at a higher angle of attack due to the vortex, both the lift and drag forces are rotated such that lift force vector generates a forward thrust and the drag force vector generates an increase in lift. With this increase in lift force, the angle of attack may be reduced to maintain the target lift needed to maintain an altitude while cruising, which causes a reduction in induced drag since drag and lift are a function of through the coefficients and .[ citation needed ]
Birds are typically observed to fly in V-shaped formations or J-shaped formations, the latter commonly known as echelon. The first study to attempt to quantify the energy saving of a large flock of birds was Lissaman & Schollenberger [6] who provided the first, albeit notably flawed, [1] estimate for a 25-member flock of birds. A most impressive 71% range extension relative to single bird flight was reported. These reported extensions are typically due to using a fixed wing approximation. Haffner (1977) experimented with birds flying in wind tunnels and calculated a range extension of a more conservative value of 22%. [7] [1]
Studies have been performed on the phase of flapping and found that birds that fly in V-shaped formations coordinate their flapping, while those in echelon do not. Willis et al (2007) found that optimal phasing of flaps accounts for 20% of power saving, suggesting that positioning is more important than perfectly caching the oncoming vortex. [8] [1]
Studies of birds have shown that the V formation can greatly enhance the overall aerodynamic efficiency by reducing the drag and thereby increasing the flight range. [9]
Insect swarms are a collective animal behavior that is an area of active research for the application of drones. The unique feature of insect swarms is their leaderless, yet organized flight. In a particle image velocimetry study of 10 midges by Kelley and Ouellette (2013), the boundaries of the swarm are statistically consistent even though the flying of the insects within the swarm are virtually asynchronous. There is also some suggestion of clustering, implying there may be some self-organizing behavior. [10]
The smallest unit of a formation is called a section or element, consisting of two aircraft; these pilots are a leader and wingman. A division or flight consists of two sections or elements. Multiple divisions or flights are assembled into a formation. [11] : 6 A standard fighter formation includes aircraft whose positions are maintained by the wingmen to within 1 mi (1.6 km) laterally and 100 ft (30 m) vertically of the flight leader's aircraft. [11] : 8 A nonstandard formation results when the flight leader has requested, and air traffic control has approved dimensions that do not conform with the stated boundaries; when operating within an authorized altitude reservation or under the provisions of a Letter of Agreement; or when flight operations are being conducted in a specially-designated airspace. [11] : 9
The fingertip four (or finger-four) is the basic four-ship formation that resembles the position of the fingertips with the hand outstretched. The flight leader (#1) is piloting the foremost aircraft (middle fingertip), with the lead's wingman (#2) to the side and trailing (index fingertip); the section lead (#3) is opposite the lead's wingman on the opposite side (ring fingertip) while the section leader's wingman (#4) is trailing the section lead towards the same side (little fingertip). The fingertip formation is designated strong right or strong left, depending on the side being flown by the section (#3 and #4) aircraft. [11] : 17 For example, viewed from overhead, the fingertip four strong right formation from left to right consists of the #2 (lead's wingman), #1 (flight leader), #3 (section lead), and #4 (section lead's wingman) aircraft.
The flight leader should decide and communicate which orientation, fingertip right or fingertip left, should be used as the basic formation prior to flight operations. Formations should transition to and from the basic formation to facilitate the use of hand and plane signals. [11] : 17
Transition | Diagram | Signal | Description & sequence | |
---|---|---|---|---|
From | To | |||
Fingertip right | Echelon right | Flight leader's left arm bent 90°, fist clenched | #3 moves section out and back, #2 crosses over to #1's right wing | |
Echelon right | Fingertip right | Flight leader's right arm bent 90°, fist clenched; #2 passes same signal to #3 | #3 moves section out to give space for #2 to cross over to #1's left wing; #3 moves section back to lead's right wing once #2 is done | |
Fingertip right | Echelon left | Flight leader's right arm bent 90°, fist clenched, two arm pumps | #3 moves section to #2's left wing, #4 crosses under #3 as the element is crossing under #2 | |
Echelon left | Fingertip right | Flight leader's left arm bent 90°, fist clenched, two arm pumps | #3 moves section to lead's right wing, #4 crosses over to #3's right wing | |
Fingertip right | Diamond | Flight leader's arm bent 90°, fist clenched; four fingers extend, then closes hand with thumb pointing rearward and motioning aft; #3 relays signal to #4; #3 signals thumbs-up to lead when complete | #4 moves into slot | |
Diamond | Fingertip right | Flight leader gently rocks wings | #4 moves from slot to #3's wing | |
Fingertip right | Trail | Flight leader gently porpoises several times; each pilot signals lead verbally when in position | #2 slides back and behind lead, followed by #3, then #4 in sequence | |
Trail | Fingertip right | Flight leader rocks wings several times, then starts shallow turn | #2 moves forward to join on lead's inside wing; #3 and #4 join as an element, then take position on lead's outside wing. |
In military aviation, tactical formation flying is the disciplined flight of two or more aircraft under the command of a flight leader. [11] : 6 Military pilots use tactical formations for mutual defense and concentration of firepower. [12] : Art 17.01
The challenge of achieving safe formation flight by unmanned aerial vehicles has been extensively investigated in the 21st century with aircraft and spacecraft systems. For aerial vehicles the advantages of performing formation flight include fuel saving, [13] improved efficiency in air traffic control and cooperative task allocation. For space vehicles precise control of formation flight may enable future large aperture space telescopes, variable baseline space interferometers, autonomous rendezvous and docking and robotic assembly of space structures.[ citation needed ] One of the simplest formations used is where autonomous aircraft maintain formation with a lead aircraft which may itself be autonomous. [14]
In civil aviation formation flying is performed at air shows or for recreation. It is used to improve flying technique and also as a prestigious activity of old aviation organizations. It represents the more challenging skill of flying near another aircraft. Formation flying proposed to reduce fuel use by minimizing drag. [15]
In the early 2000s, NASA's Autonomous Formation Flight program used a pair of F/A-18s. In 2013, the Air Force Research Laboratory's Surfing Aircraft Vortices for Energy project showed 10–15% in fuel savings, installed on two Boeing C-17 Globemaster IIIs. In 2017, NASA measured 8–10% lower fuel flow with two Gulfstream III aircraft on wake surfing test flights. In 2018, the ecoDemonstrator, a Boeing 777F freighter from FedEx Express, had its fuel consumption reduced by 5–10% with the autopilot maintaining the 4,000 ft (1.2 km) separation based on ADS-B and TCAS information. [16]
By taking advantage of wake updraft like migrating birds (biomimicry), Airbus believes an aircraft can save 5–10% of fuel by flying 1.5–2 nmi (2.8–3.7 km) behind the preceding one. After Airbus A380s tests showing 12% savings, it launched its 'fello'fly' project in November 2019 for test flights in 2020 with two A350s, before transatlantic flight trials with airlines in 2021. Certification for shorter separation is enabled by ADS-B in oceanic airspace, and the only modification required would be flight control systems software. Comfort would not be affected and trials are limited to two aircraft to reduce complexity but the concept could be expanded to include more. Commercial operations could begin in 2025 with airline schedule adjustments, and other manufacturers' aircraft could be included. [17]
On 9 November 2021, Airbus performed a 7 h 40 min Toulouse-Montreal demonstration with an A350-900 and A350-1000 separated by 3 km (1.6 nmi), saving over 6 t (13,000 lb) of carbon dioxide: a potential of more than 5% fuel savings. [18] Partly funded by the EU SESAR air traffic management research, Airbus' Geese initiative will include Air France and French Bee A350s for flight trials in 2025 to 2026, and will include Boeing for interoperability. [19]
In fluid dynamics, a stall is a reduction in the lift coefficient generated by a foil as angle of attack exceeds its critical value. The critical angle of attack is typically about 15°, but it may vary significantly depending on the fluid, foil – including its shape, size, and finish – and Reynolds number.
Flight or flying is the process by which an object moves through a space without contacting any planetary surface, either within an atmosphere or through the vacuum of outer space. This can be achieved by generating aerodynamic lift associated with gliding or propulsive thrust, aerostatically using buoyancy, or by ballistic movement.
In aeronautics, the aspect ratio of a wing is the ratio of its span to its mean chord. It is equal to the square of the wingspan divided by the wing area. Thus, a long, narrow wing has a high aspect ratio, whereas a short, wide wing has a low aspect ratio.
An airfoil or aerofoil is a streamlined body that is capable of generating significantly more lift than drag. Wings, sails and propeller blades are examples of airfoils. Foils of similar function designed with water as the working fluid are called hydrofoils.
In aerodynamics, the lift-to-drag ratio is the lift generated by an aerodynamic body such as an aerofoil or aircraft, divided by the aerodynamic drag caused by moving through air. It describes the aerodynamic efficiency under given flight conditions. The L/D ratio for any given body will vary according to these flight conditions.
Lift-induced drag, induced drag, vortex drag, or sometimes drag due to lift, in aerodynamics, is an aerodynamic drag force that occurs whenever a moving object redirects the airflow coming at it. This drag force occurs in airplanes due to wings or a lifting body redirecting air to cause lift and also in cars with airfoil wings that redirect air to cause a downforce. It is symbolized as , and the lift-induced drag coefficient as .
Wingtip devices are intended to improve the efficiency of fixed-wing aircraft by reducing drag. Although there are several types of wing tip devices which function in different manners, their intended effect is always to reduce an aircraft's drag. Wingtip devices can also improve aircraft handling characteristics and enhance safety for following aircraft. Such devices increase the effective aspect ratio of a wing without greatly increasing the wingspan. Extending the span would lower lift-induced drag, but would increase parasitic drag and would require boosting the strength and weight of the wing. At some point, there is no net benefit from further increased span. There may also be operational considerations that limit the allowable wingspan.
Aviation is the design, development, production, operation, and use of aircraft, especially heavier-than-air aircraft. Articles related to aviation include:
A slipstream is a region behind a moving object in which a wake of fluid is moving at velocities comparable to that of the moving object, relative to the ambient fluid through which the object is moving. The term slipstream also applies to the similar region adjacent to an object with a fluid moving around it. "Slipstreaming" or "drafting" works because of the relative motion of the fluid in the slipstream.
Wingtip vortices are circular patterns of rotating air left behind a wing as it generates lift. The name is a misnomer because the cores of the vortices are slightly inboard of the wing tips. Wingtip vortices are sometimes named trailing or lift-induced vortices because they also occur at points other than at the wing tips. Indeed, vorticity is trailed at any point on the wing where the lift varies span-wise ; it eventually rolls up into large vortices near the wingtip, at the edge of flap devices, or at other abrupt changes in wing planform.
An airplane or aeroplane, informally plane, is a fixed-wing aircraft that is propelled forward by thrust from a jet engine, propeller, or rocket engine. Airplanes come in a variety of sizes, shapes, and wing configurations. The broad spectrum of uses for airplanes includes recreation, transportation of goods and people, military, and research. Worldwide, commercial aviation transports more than four billion passengers annually on airliners and transports more than 200 billion tonne-kilometers of cargo annually, which is less than 1% of the world's cargo movement. Most airplanes are flown by a pilot on board the aircraft, but some are designed to be remotely or computer-controlled such as drones.
A V formation is a symmetric V- or chevron-shaped flight formation. In nature, it occurs among geese, swans, ducks, and other migratory birds, improving their energy efficiency, while in human aviation, it is used mostly in military aviation, air shows, and occasionally commercial aviation.
A vertical stabilizer or tail fin is the static part of the vertical tail of an aircraft. The term is commonly applied to the assembly of both this fixed surface and one or more movable rudders hinged to it. Their role is to provide control, stability and trim in yaw. It is part of the aircraft empennage, specifically of its stabilizers.
In fluid dynamics, drag, sometimes referred to as fluid resistance, is a force acting opposite to the relative motion of any object moving with respect to a surrounding fluid. This can exist between two fluid layers, two solid surfaces, or between a fluid and a solid surface. Drag forces tend to decrease fluid velocity relative to the solid object in the fluid's path.
A blended wing body (BWB), also known as blended body, hybrid wing body (HWB) or a lifting aerofoil fuselage, is a fixed-wing aircraft having no clear dividing line between the wings and the main body of the craft. The aircraft has distinct wing and body structures, which are smoothly blended together with no clear dividing line. This contrasts with a flying wing, which has no distinct fuselage, and a lifting body, which has no distinct wings. A BWB design may or may not be tailless.
The maximal total range is the maximum distance an aircraft can fly between takeoff and landing. Powered aircraft range is limited by the aviation fuel energy storage capacity considering both weight and volume limits. Unpowered aircraft range depends on factors such as cross-country speed and environmental conditions. The range can be seen as the cross-country ground speed multiplied by the maximum time in the air. The fuel time limit for powered aircraft is fixed by the available fuel and rate of consumption.
An adaptive compliant wing is a wing which is flexible enough for aspects of its shape to be changed in flight. Flexible wings have a number of benefits. Conventional flight control mechanisms operate using hinges, resulting in disruptions to the airflow, vortices, and in some cases, separation of the airflow. These effects contribute to the drag of the aircraft, resulting in less efficiency and higher fuel costs. Flexible aerofoils can manipulate aerodynamic forces with less disruptions to the flow, resulting in less aerodynamic drag and improved fuel economy.
Delta formation is a flight pattern where multiple flying objects will come together in a V in order to fly more efficiently. Each trailing object is positioned slightly higher than the one in front, and uses the air moved by the forward object to reduce wind resistance.
The fuel economy in aircraft is the measure of the transport energy efficiency of aircraft. Fuel efficiency is increased with better aerodynamics and by reducing weight, and with improved engine brake-specific fuel consumption and propulsive efficiency or thrust-specific fuel consumption. Endurance and range can be maximized with the optimum airspeed, and economy is better at optimum altitudes, usually higher. An airline efficiency depends on its fleet fuel burn, seating density, air cargo and passenger load factor, while operational procedures like maintenance and routing can save fuel.
Skin friction drag is a type of aerodynamic or hydrodynamic drag, which is resistant force exerted on an object moving in a fluid. Skin friction drag is caused by the viscosity of fluids and is developed from laminar drag to turbulent drag as a fluid moves on the surface of an object. Skin friction drag is generally expressed in terms of the Reynolds number, which is the ratio between inertial force and viscous force.