Translation and Meaning of stalling, Definition of stalling in Almaany Online Dictionary of English-German. Worterbuch, Wörterbuch, Deutsch, Wörterbücher. Übersetzung für 'stalling' im kostenlosen Englisch-Deutsch Wörterbuch und viele weitere Deutsch-Übersetzungen. Übersetzung im Kontext von „stalling“ in Englisch-Deutsch von Reverso Context: Indeed, the U-2 has to be flown at near maximum speed to avert stalling.
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speed [AVIAT.]. relight.nu | Übersetzungen für 'stalling' im Englisch-Deutsch-Wörterbuch, mit echten Sprachaufnahmen, Illustrationen, Beugungsformen. (ii) a maximum stalling speed in the landing configuration (VS0) [ ]. Übersetzung Englisch-Deutsch für stalling im PONS Online-Wörterbuch nachschlagen! Gratis Vokabeltrainer, Verbtabellen, Aussprachefunktion. stalling Bedeutung, Definition stalling: 1. present participle of stall 2. If an engine stalls, or if you stall it, it stops working. Übersetzung im Kontext von „stalling“ in Englisch-Deutsch von Reverso Context: Indeed, the U-2 has to be flown at near maximum speed to avert stalling. Übersetzung für 'stalling' im kostenlosen Englisch-Deutsch Wörterbuch und viele weitere Deutsch-Übersetzungen.
Übersetzung Englisch-Deutsch für stalling im PONS Online-Wörterbuch nachschlagen! Gratis Vokabeltrainer, Verbtabellen, Aussprachefunktion. stalling Bedeutung, Definition stalling: 1. present participle of stall 2. If an engine stalls, or if you stall it, it stops working. Übersetzung für 'stalling' im kostenlosen Englisch-Deutsch Wörterbuch und viele weitere Deutsch-Übersetzungen. DE Bude Marktbude Marktstand. Jahrhunderts erbaut und ist Partyspiele Brettspiele jeher ein symbolischer Ort des Handels: in der Vergangenheit wurden hier Seide und kostbare Gegenstände verkauft, während er heute durch die Bingo Spielen Lubeck mit Lederwaren und Souvenir…. Wählen Sie ein Wörterbuch aus. English So why was I stalling? Binding to these Neu De Test is thought to elicit either futile cycles of mismatch repair or replication William Hill Online Casinowhich can lead to cell death. Ibiza Town Anmelden Spiele designer boutiques while hippy markets are held across the island, with unique stalls offering everything from local handicrafts to handmade jewellery, art and clothes. Hallo Download Go Wild Casino. Italienisch Wörterbücher. Übersetzung für 'stalling' im kostenlosen Englisch-Deutsch Wörterbuch von LANGENSCHEIDT – mit Beispielen, Synonymen und Aussprache. stalling ist eine flektierte Form von stall. Alle weiteren Informationen findest du im Haupteintrag stall. Bitte nimm Ergänzungen deshalb auch nur dort vor. Translation and Meaning of stalling, Definition of stalling in Almaany Online Dictionary of English-German. Worterbuch, Wörterbuch, Deutsch, Wörterbücher.
Stalling Navigation menu VideoLearner Car Stalling Binding to these proteins is thought to elicit either futile cycles of mismatch repair or replication stallingwhich Stalling lead to cell death. English So why was I stalling? Ibiza Town boasts designer boutiques while hippy markets are held across the island, with unique stalls Free Roulette Wheel Game everything from local handicrafts to handmade jewellery, art and Free Roulete. An vielen kleinen Verkaufsständen werden Speider Man Spiele, Kerzen, Christbaumschmuck und weihnächtliche Geschenkartikel feil geboten. The farmers' market stalls and the Thaur farmers' store also supply food and drink, notably the Austrian Dietary Chefs who prepare original dishes from radishes. Viele Millionen der knackigen Knollen werden hier jedes Jahr gebündelt. It is time for the Commission and Member States to stop stalling '. Rathauspark During those events, Rathausplatz is crammed with stalls selling food and drinks, and - in case of the Christkindlmarkt - Christmas decorations and presents. Lass uns in Kontakt bleiben. There is also a large number Desertoperations bars, pubs and restaurants, where travelers from all over the world, and increasing the young Thais too, meet, dance, drink, chat, flirt or watch videos until the early hours. Some aircraft may be subject to post-stall gyration e. The angle at which this occurs is called the critical angle of attack. For Kartenspiel Solitaire Download trailing-edge stall, separation begins at small angles of attack near the trailing William Hill Online Casino of the wing while the rest of the flow over the wing remains attached. However, if the aircraft is turning or pulling up from a dive, additional lift is required to provide the vertical or lateral acceleration, and so the stall speed is higher. February Typical values both Slotkings the range of deep stall, as defined above, and the locked-in trim point are given for the Douglas DC-9 Series 10 by Schaufele.
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Want to learn more? A car may stall due to the driver braking too suddenly. I stalled the car twice during my driving test but still managed to pass.
Machines - not functioning. She says she'll give me the money next week but I think she's just stalling for time. I managed to stall him for a few days until I'd got enough money to pay back the loan.
Japan's economic growth has stalled, with industrial production contracting in June for the fourth straight month. Commandos stalled the enemy attack by destroying three bridges.
Fears are growing that a tax increase may stall economic recovery. Delaying and wasting time. You can also find related words, phrases, and synonyms in the topics: Economics.
Examples of stalling. In a few cases, a complete second unit of living and stalling compartments appears to have been added to a house figure 3d.
From the Cambridge English Corpus. To avoid the problem of stalling acceleration, we introduced a phase delay. These examples are from the Cambridge English Corpus and from sources on the web.
Any opinions in the examples do not represent the opinion of the Cambridge Dictionary editors or of Cambridge University Press or its licensors.
The two remaining groups were similar in their frequencies of succeeding and stalling. However, consistent preferences among voters have a marked impact on convergence patterns, with convergence rates stalling around the fourth election period.
Some resources come from other than self or spouse and not stalling! Binding to these proteins is thought to elicit either futile cycles of mismatch repair or replication stalling , which can lead to cell death.
These reforms achieved only moderate results, stalling after a few years. If the cuttings are not cleared quickly, they will be ground down, reducing drilling efficiency and causing excessive drill bit wear or bit stalling in an extreme case.
In fluid dynamics , a stall is a reduction in the lift coefficient generated by a foil as angle of attack increases. The critical angle of attack is typically about 15 degrees, but it may vary significantly depending on the fluid, foil, and Reynolds number.
Stalls in fixed-wing flight are often experienced as a sudden reduction in lift as the pilot increases the wing's angle of attack and exceeds its critical angle of attack which may be due to slowing down below stall speed in level flight.
A stall does not mean that the engine s have stopped working, or that the aircraft has stopped moving—the effect is the same even in an unpowered glider aircraft.
Vectored thrust in manned and unmanned aircraft is used to maintain altitude or controlled flight with wings stalled by replacing lost wing lift with engine or propeller thrust, thereby giving rise to post-stall technology.
Because stalls are most commonly discussed in connection with aviation , this article discusses stalls as they relate mainly to aircraft, in particular fixed-wing aircraft.
The principles of stall discussed here translate to foils in other fluids as well. A stall is a condition in aerodynamics and aviation such that if the angle of attack increases beyond a certain point, then lift begins to decrease.
The angle at which this occurs is called the critical angle of attack. This angle is dependent upon the airfoil section or profile of the wing, its planform , its aspect ratio , and other factors, but is typically in the range of 8 to 20 degrees relative to the incoming wind "relative wind" for most subsonic airfoils.
Stalling is caused by flow separation which, in turn, is caused by the air flowing against a rising pressure. For the trailing-edge stall, separation begins at small angles of attack near the trailing edge of the wing while the rest of the flow over the wing remains attached.
As angle of attack increases, the separated regions on the top of the wing increase in size as the flow separation moves forward, and this hinders the ability of the wing to create lift.
The separated flow usually causes buffeting. Piston-engined and early jet transports had very good stall behaviour with pre-stall buffet warning and, if ignored, a straight nose-drop for a natural recovery.
Wing developments that came with the introduction of turbo-prop engines introduced unacceptable stall behaviour. Leading-edge developments on high-lift wings, and the introduction of rear-mounted engines and high-set tailplanes on the next generation of jet transports, also introduced unacceptable stall behaviour.
The probability of achieving the stall speed inadvertently, a potentially hazardous event, had been calculated, in , at about once in every , flights,  often enough to justify the cost of development of warning devices, such as stick shakers, and devices to automatically provide an adequate nose-down pitch, such as stick pushers.
When the mean angle of attack of the wings is beyond the stall a spin , which is an autorotation of a stalled wing, may develop.
A spin follows departures in roll, yaw and pitch from balanced flight. For example, a roll is naturally damped with an unstalled wing, but with wings stalled the damping moment is replaced with a propelling moment.
The graph shows that the greatest amount of lift is produced as the critical angle of attack is reached which in earlyth century aviation was called the "burble point".
This angle is Symmetric airfoils have lower critical angles but also work efficiently in inverted flight.
The graph shows that, as the angle of attack exceeds the critical angle, the lift produced by the airfoil decreases. The information in a graph of this kind is gathered using a model of the airfoil in a wind tunnel.
Because aircraft models are normally used, rather than full-size machines, special care is needed to make sure that data is taken in the same Reynolds number regime or scale speed as in free flight.
The separation of flow from the upper wing surface at high angles of attack is quite different at low Reynolds number from that at the high Reynolds numbers of real aircraft.
In particular at high Reynolds numbers the flow tends to stay attached to the airfoil for longer because the inertial forces are dominant with respect to the viscous forces which are responsible for the flow separation ultimately leading to the aerodynamic stall.
For this reason wind tunnel results carried out at lower speeds and on smaller scales models of the real life counterparts often tend to overestimate the aerodynamic stall angle of attack .
High-pressure wind tunnels are one solution to this problem. In general, steady operation of an aircraft at an angle of attack above the critical angle is not possible because, after exceeding the critical angle, the loss of lift from the wing causes the nose of the aircraft to fall, reducing the angle of attack again.
This nose drop, independent of control inputs, indicates the pilot has actually stalled the aircraft. This graph shows the stall angle, yet in practice most pilot operating handbooks POH or generic flight manuals describe stalling in terms of airspeed.
This is because all aircraft are equipped with an airspeed indicator , but fewer aircraft have an angle of attack indicator. An aircraft's stalling speed is published by the manufacturer and is required for certification by flight testing for a range of weights and flap positions, but the stalling angle of attack is not published.
As speed reduces, angle of attack has to increase to keep lift constant until the critical angle is reached. The airspeed at which this angle is reached is the 1g, unaccelerated stalling speed of the aircraft in that particular configuration.
A fixed-wing aircraft can be made to stall in any pitch attitude or bank angle or at any airspeed but deliberate stalling is commonly practiced by reducing the speed to the unaccelerated stall speed, at a safe altitude.
Unaccelerated 1g stall speed varies on different fixed-wing aircraft and is represented by colour codes on the airspeed indicator. As the plane flies at this speed, the angle of attack must be increased to prevent any loss of altitude or gain in airspeed which corresponds to the stall angle described above.
The pilot will notice the flight controls have become less responsive and may also notice some buffeting, a result of the turbulent air separated from the wing hitting the tail of the aircraft.
In most light aircraft , as the stall is reached, the aircraft will start to descend because the wing is no longer producing enough lift to support the aircraft's weight and the nose will pitch down.
Recovery from the stall involves lowering the aircraft nose, to decrease the angle of attack and increase the air speed, until smooth air-flow over the wing is restored.
Normal flight can be resumed once recovery is complete. It is taught and practised in order for pilots to recognize, avoid, and recover from stalling the aircraft.
The only dangerous aspect of a stall is a lack of altitude for recovery. A special form of asymmetric stall in which the aircraft also rotates about its yaw axis is called a spin.
A spin can occur if an aircraft is stalled and there is an asymmetric yawing moment applied to it. The net effect is that one wing is stalled before the other and the aircraft descends rapidly while rotating, and some aircraft cannot recover from this condition without correct pilot control inputs which must stop yaw and loading.
The most common stall-spin scenarios occur on takeoff departure stall and during landing base to final turn because of insufficient airspeed during these maneuvers.
Stalls also occur during a go-around manoeuvre if the pilot does not properly respond to the out-of-trim situation resulting from the transition from low power setting to high power setting at low speed.
Stalls occur not only at slow airspeed, but at any speed when the wings exceed their critical angle of attack. Attempting to increase the angle of attack at 1g by moving the control column back normally causes the aircraft to climb.
However, aircraft often experience higher g-forces, such as when turning steeply or pulling out of a dive. In these cases, the wings are already operating at a higher angle of attack to create the necessary force derived from lift to accelerate in the desired direction.
Increasing the g-loading still further, by pulling back on the controls, can cause the stalling angle to be exceeded, even though the aircraft is flying at a high speed.
Different aircraft types have different stalling characteristics but they only have to be good enough to satisfy their particular Airworthiness authority.
For example, the Short Belfast heavy freighter had a marginal nose drop which was acceptable to the Royal Air Force. When the aircraft were sold to a civil operator they had to be fitted with a stick pusher to meet the civil requirements.
For example, first generation jet transports have been described as having an immaculate nose drop at the stall. These are described in "Warning and safety devices".
Stalls depend only on angle of attack, not airspeed. This speed is called the "stall speed". An aircraft flying at its stall speed cannot climb, and an aircraft flying below its stall speed cannot stop descending.
Any attempt to do so by increasing angle of attack, without first increasing airspeed, will result in a stall. The actual stall speed will vary depending on the airplane's weight, altitude, configuration, and vertical and lateral acceleration.
Speed definitions vary and include:. An airspeed indicator, for the purpose of flight-testing, may have the following markings: the bottom of the white arc indicates V S0 at maximum weight, while the bottom of the green arc indicates V S1 at maximum weight.
While an aircraft's V S speed is computed by design, its V S0 and V S1 speeds must be demonstrated empirically by flight testing. The normal stall speed, specified by the V S values above, always refers to straight and level flight, where the load factor is equal to 1g.
However, if the aircraft is turning or pulling up from a dive, additional lift is required to provide the vertical or lateral acceleration, and so the stall speed is higher.
An accelerated stall is a stall that occurs under such conditions. In a banked turn , the lift required is equal to the weight of the aircraft plus extra lift to provide the centripetal force necessary to perform the turn:  .
To achieve the extra lift, the lift coefficient , and so the angle of attack, will have to be higher than it would be in straight and level flight at the same speed.
Therefore, given that the stall always occurs at the same critical angle of attack,  by increasing the load factor e.
The table that follows gives some examples of the relation between the angle of bank and the square root of the load factor.
According to Federal Aviation Administration FAA terminology, the above example illustrates a so-called turning flight stall , while the term accelerated is used to indicate an accelerated turning stall only, that is, a turning flight stall where the airspeed decreases at a given rate.
Accelerated stalls also pose a risk in powerful propeller aircraft with a tendency to roll in reaction to engine torque.
When such an aircraft is flying close to its stall speed in straight and level flight, the sudden application of full power may roll the aircraft and create the same aerodynamic conditions that induce an accelerated stall in turning flight.
An aircraft that displays this rolling tendency is the Mitsubishi MU-2 ; pilots of this aircraft are trained to avoid sudden and drastic increases in power at low altitude and low airspeed, as an accelerated stall under these conditions is very difficult to safely recover from.
A notable example of an air accident involving a low-altitude turning flight stall is the Fairchild Air Force Base B crash.
Dynamic stall is a non-linear unsteady aerodynamic effect that occurs when airfoils rapidly change the angle of attack. The rapid change can cause a strong vortex to be shed from the leading edge of the aerofoil, and travel backwards above the wing.
As soon as it passes behind the trailing edge, however, the lift reduces dramatically, and the wing is in normal stall.
Dynamic stall is an effect most associated with helicopters and flapping wings, though also occurs in wind turbines  , and due to gusting airflow.
During forward flight, some regions of a helicopter blade may incur flow that reverses compared to the direction of blade movement , and thus includes rapidly changing angles of attack.
Oscillating flapping wings, such as those of insects like the bumblebee —may rely almost entirely on dynamic stall for lift production, provided the oscillations are fast compared to the speed of flight, and the angle of the wing changes rapidly compared to airflow direction.
Stall delay can occur on airfoils subject to a high angle of attack and a three-dimensional flow. When the angle of attack on an airfoil is increasing rapidly, the flow will remain substantially attached to the airfoil to a significantly higher angle of attack than can be achieved in steady-state conditions.
As a result, the stall is delayed momentarily and a lift coefficient significantly higher than the steady-state maximum is achieved. The effect was first noticed on propellers.
A deep stall or super-stall is a dangerous type of stall that affects certain aircraft designs,  notably jet aircraft with a T-tail configuration and rear-mounted engines.
In these designs, the turbulent wake of a stalled main wing, nacelle-pylon wakes and the wake from the fuselage  "blanket" the horizontal stabilizer, rendering the elevators ineffective and preventing the aircraft from recovering from the stall.
Taylor  states T-tail propeller aircraft, unlike jet aircraft, do not usually require a stall recovery system during stall flight testing due to increased airflow over the wing root from the prop wash.
Nor do they have rear mounted nacelles which can contribute substantially to the problem. He also gives a definition that relates deep stall to a locked-in condition where recovery is impossible.