Lightning direct effects handbook wichita state university. The sea or the ground in this case, has to have waves for the bird to glide they cant flap and fly. Airplane upset prevention and recovery training aid icao. Ground effect one of the most misunderstood aerodynamic effects is called ground effect. Experimental investigation of a winginground effect craft. Attitudes to noise from aviation sources in england anase pdf. The effect of ground effect is likened to floating above the ground especially when landing. Simulated tiltrotor aircraft operation in close proximity. Furthermore, the effect of turbulence on ground interference is usually ignored. Modeling of ground reflection effects in aircraft flyover noise synthesi s problem area in the case of generating artificial aircraft noise, also called aircraft noise synthesis, the ground interference effect is often simulated by plane wave reflection coefficients.
While ground effect might cause you headaches when you land, its the exact opposite for other planes. A groundeffect vehicle is a combination of a maritime vessel and an aircraft. When landing, ground effect can give the pilot the feeling that the aircraft is floating. The boeing pelican ultra ultra large transport aircraft was a proposed ground effect fixedwing aircraft under study by boeing phantom works. The impact of new technologies on future co2 emissions of the global aviation fleet is. Subarupowered homemade hoverwing is a diy miniekranoplan. Force measurement on aircraft model with and without. The aerodynamic characteristics of the winginground effect wig craft model that has a noble configuration of a compound wing was experimentally investigated and universiti teknologi malaysia utm wind tunnel with and without endplates. It can only travel over a more or less smooth surface like the ground, water, or ice, flying several meters above it to produce more lift force and less drag than any fixedwing aircraft generates close to the ground.
Data for the tests in the lockheed tunnel were obtained from reference 2. Autonomous landing of quadrotor based on ground effect modelling. Pdf aerodynamics of a cambered airfoil in ground effect. Change in f15 lift coefficient because of ground effect as a function of height. But the range would be greatly reduced to 6,500 nautical miles when not using the ground effect. Although a large body of research results is now available. The effective angle of attack also increases giving an increase in lift and a floating tendancy. Principle plays in the ability of aircraft to achieve lift, the bernoulli principle is not the only reason for. This is the result of a phenomenon which is better known than understood even by some experienced pilots. In very broad terms, aircraft fly because the movement of the wing through the air produces a greater static pressure on the lower surface of the wing than on the upper surface of the wing.
Young1 nasa ames research center, moffett field, ca, 94035 a midfidelity computational fluid dynamics tool called rotcfd specifically developed. This configuration wont be stable as a regular aircraft, but you are not trying to do that. A helicopter committed to ground effect flight only is an easier way to go, just make it safer. The basic design principle is that the closer the wing operates to an external surface such as the ground, when it is said to be in ground effect, the more efficient it becomes. Structural ice is the stuff that sticks to the outside of the airplane. Normally, some of the highpressure air beneath the wing wraps around to the lowpressure top of the wing. Thus flying in ground effect ige potentially offers a very economical form of rapid transport. The albatross has two ways of gliding both of which use the wind reflected off waves of the sea. This reduces induced drag and for a given thrust setting the aircraft will tend to speed up.
Groundeffect analysis of a jet transport airplane author. It is possible to fly an airplane just clear of the ground or water at a slightly slower airspeed than that required to sustain level flight at higher altitudes. Understand the effect of air flowing over a curved surface. Lift and drag forces, pitching moment coefficients, and the centre of pressure were measured with respect to the ground clearance and the wing angle of. Overestimated aircraft stall angle of attack, setting the aircraft stall warning system too high to warn the crew of stall. For ground effect aircraft, the positive lift is directed upward and away from the ground. Aerodynamics of a cambered airfoil in ground effect article pdf available in international journal of fluid mechanics research 322. Aircraft noise pollution is a harmful noise effect produced by aircraft in flight. Force measurement on aircraft model with and without winglet using low speed wind tunnel n. Senthilkumar3 1professor,department of aeronautical engineering, rajalakshmi engineering college, chennai602105,india email. For decades the russians have experimented with aircraft they called wig wing in groundeffect planes. The landing distance will therefore tend to increase.
For fixedwing aircraft, ground effect is the increased lift and decreased aerodynamic drag that. Seastryders revolutionary design may be operated as a class c ground effect craft according to the international maritime organizations imo ruling on this type of craft. Flightmeasured ground effect on a lowaspectratio ogee. Model of effects of aircraft noise on communities non acoustic factors acoustic factors shortterm effects longterm effects complaints other public action sleep disturbance speech interference activity interference short term annoyance. Ground effect one of the most misunderstood aerodynamic. The goal of this project is to build a modelsized aircraft capable of flying close to the ground or hovering right above it. Many of the gev articles focus on increased lift in ground effect, which can give the reader the wrong idea about aircraft operations in the same regime.
Consequently, induced drag increases due to greater wingtip vortices meaning that the aircraft performance is affected and it will not perform as well in free air as it will in ground effect. This effect is a consequence of the distortion of the airflow below such surfaces attributable to the proximity of the ground. Intended as a largecapacity transport craft for military or civilian use, it would have a wingspan of 500 feet 150 m, a cargo capacity of 1,400 tons. While the pelican is yet to become a prototype the concept is hardly a new one.
Modeling of ground reflection effects in aircraft flyover. The flightmeasured ground effect characteristics of the test aircraft are described in this report and the various windtunnel data are compared with the flight data. Whether a cg is more aft or more forward makes all the difference in the world. The russian ones didnt have any anhedral or dihedral. Pelham phillips langley research center summary some results of a study of the influence of groundinduced aerodynamic. The pilot can then fly just above the runway while the aircraft accelerates in ground effect until a safe climb speed is reached. The downwash from the wings and the downward component of the wingtip vortices create a higher than normal pressure area below the wings because the air hits the ground and cant escape, increasing lift. Ground effect can be divided up into two distinct regimes, ram and normal ground effect 1.
Flight 77 was not trying to land, nor in a flare, nor at approach speed, thus no high angle of attack. Liftis a force that is produced by the dynamic effect of the air acting on the airfoil, and acts perpendicular to the flight path through the center of lift cl and. Part boat, part hovercraft, when travelling at speed this craft generates enough lift from its stub wings to fly 15 to 30 centimeters above the water. This handbook is intended to assist aircraft design and certification engineers in protecting small personal aircraft against the direct effects of lightning strikes. Ram ground effect occurs where the wing is at an altitude of hc0. Simulated tiltrotor aircraft operation in close proximity to a building in wind and groundeffect conditions larry a.
Hence, the closer a community is with respect to the airport runway, the larger this asymmetrical effect will be. Applicability the current prediction methodology is readily integrated in nlrs doc. As can be seen, the type of aircraft also has a strong effect, with flying boats having the highest emptyweight fractions and longrange military aircraft having the. The lippisch configuration was chosen because of its supposed greater inherent stability when moving between in ground effect ige and out of ground effect oge.
When all of these benefits are taken into account, we find that a vehicle operating in ground effect has the potential to be much more efficient than an aircraft operating at high altitude. In many general aviation airplanes this effect produces greater lift and less drag for a given angle of attack. The aquaglide is a fiveseat wing in groundeffect vehicle powered by a gasoline engine. The aerodynamic efficiency of an aircraft is expressed through a quantity called the lifttodrag ratio, or ld. Ground effect, controlled impact demonstration, jet transport, boeing72 0. Motion rc merchandise paint, covering, graphics pilot figures. Dynamic ground effects flight test of an f15 aircraft. Wing in ground effect wig not to be confused with ground effect in auto racing explained in this article aircraft may be affected by a number of ground effects, or aerodynamic effects due to a flying bodys proximity to the ground. The investigations conducted in recent years show distinctly lower guide values for health hazards, learning difficulties, and annoyance than previous assumptions on which the german aircraft noise act is also based. Thus our main guideline is to exploit ground effect to a maximum in. The aquaglide 5 is a fiveseat wing in groundeffect. Causes for discrepancies in ground effect analyses.
A groundeffect vehicle needs some forward velocity to produce lift dynamically and the principal benefit of operating a wing in ground effect is to reduce its liftdependent drag. While true, remember that gevs wings are much closer to the ground than an aircrafts wing and the goal of the aircraft is different. Wing in ground effect the conventional practical use of lifting bodies, are wings on aircraft. The pilot can then fly just above the runway while the aircraft. I have taught flight students how to use ground effect to advantage in landing a fixed wing aircraft. Its impossible to give a correct and simple explanation i think. When taking off, ground effect may temporarily reduce the stall speed. As an airplane climbs out of ground effect on takeoff the lifting ability of the wing decreases for the same angle of attack. The wingtip vortices streaming behind an aircraft follow a downward inclined path for some distance behind the aircraft and then gradually level out to follow a path at a lower level than the aircraft and also drift apart. Used a flawed assumption for maximum lift coefficient in ground effect, calculating a minimum safe takeoff speed too low to be achievable. Ground effect hi aileron when an aircraft enters ground effect the wing tip vortices are restricted. The dynamics of aircraft rotation and liftoff and its. Ground effect refers to the increased lift and decreased drag that an aircraft wing generates when an aircraft is about one wingspans length or less over the ground or surface. Some aircraft, like the russian ekranoplan, were designed to only fly in ground effect, and never get higher than a few feet from the earths surface, allowing them to carry a lot more payload than what would normally be possible.
Mk1 powered by a model aircraft cox 049 engine figure 2. Health hazards caused by aircraft noise can be most reliably identified from epidemiological field studies. Ground effect is the increased lift generated by wings when the aircraft is close to the ground. Rather it is my intention to explain the correct information in a way that arms you the pilot with an understanding that aids you in flying the craft of piloting a fixed wing aircraft in a safe and controlled manner. Autonomous landing of quadrotor based on ground effect. The effect of elevator manipulation ground clearance requirements for simultaneous pitching and banking after liftoff discussion determination of vertical velocity at the moment of liftoff aircraft response following liftoff, ignoring elevator lift aircraft response to elevator control during flareup. Ground effect on rotary aircraft has been studied for many decades. Including atmospheric propagation effects in aircraft take. Ground effects related to landing of airplanes with lowaspectratiowings by william b.
My design of helicopter ground effect vehicle is much different to the usual and because i must get others to do work for me that creates the situation that you have skeptics on the projects which will insure that you finish up with a lemon. Ground effects related to landing of airplanes with low. It is the phenomena when an airfoil is operating close to a boundary such as the ground or water. For fixedwing aircraft, ground effect is the increased lift and decreased aerodynamic drag that an aircrafts wings generate when they are close to a fixed surface. Download fulltext pdf download fulltext pdf download fulltext pdf experimental investigation of a winginground effect craft article pdf available in the scientific world journal 2014. For an engineering project, we need to design and study a working ground effect plane. Ground effect is the name given to the positive influence on the lifting characteristics of the horizontal surfaces of an aircraft wing when it is close to the ground. It is also intended to assist federal aviation administration faa certifying engineers in assessing the adequacy of proposed lightning protection designs. Many airplane upsets occur while the pilot is engaged in some task that takes attention away from the flight instruments.
267 841 1285 1550 225 673 1017 193 293 1590 1100 1391 185 841 210 839 1586 553 1056 963 1431 910 285 1515 1043 756 59 1663 1372 13 31 1370 580 1046 355 1287 670 699 1074