Low-g condition

 ( Aerodynamics ) 

Low- g condition is a phase of aerodynamic flight where the airframe is temporarily unloaded. The pilot and the airframe feel temporarily "Weightlessness" because the aircraft is in free-fall or decelerating vertically at the top of a climb. It may also occur during an excessively rapid entry into autorotation. This can have a disastrous effect on the aircraft, particularly in the case of helicopters, some of which need the rotor to constantly be under a non-zero amount of load.

Low-g conditions are forbidden for teetering rotor helicopters, because the design cannot control its attitude independently and can also be dangerous for other types. The U.S. Army discovered the danger of Low-g conditions in the 1960s when they were losing helicopters to mysterious accidents that did not have a clear cause.

Low-g conditions is a term related to flight, and related terms are zero g conditions and negative g. Low-g conditions can cause an environment where mast bumping in helicopters may occur.

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Effects

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Smaller airplanes Most smaller airplanes and gliders have no problems with 0  g conditions. In fact, it can be enjoyable to have zero gravity in the cockpit. To produce 0  g, the aircraft has to follow a ballistic flight path, which is essentially an upside down parabola. This is the only method to simulate zero gravity for humans on earth.

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Helicopters In contrast, low-g conditions can be disastrous for . In such a situation their helicopter rotor may flap beyond normal limits. The excessive flapping can cause the root of the blades to exceed the limit of their hinges and this condition, known as mast bumping, can cause the separation of the blades from the hub or for the mast to shear, and hence detach the whole system from the aircraft, falling from the sky. This is especially true for helicopters with , such as the two-blade design seen on Robinson helicopters. This effect was first discovered when many accidents with Bell UH-1 and AH-1 helicopters occurred. These particular helicopters simply crashed without any obvious cause. Later, it was found that these accidents usually happened during low terrain flight after passing a ridge and initiating a dive from the previous climb. Articulated and rigid rotor systems do not lose controlling forces up to 0  g, but may encounter this depending on their flapping hinge offset from the mast.

Dangerous situations can occur in helicopters in low-g conditions, especially teetering rotors designs. In the late 1960s the US Army discovered the danger of a main rotor striking a helicopter's own tail, in certain aerodynamic conditions particularly Low-g conditions. During low-g conditions the weight of the helicopter is unloaded from the main rotor and inputs to the controls can create a dangerous situation at that time.

Helicopters with teetering rotors—for must not be subjected to a low-g condition, because such rotor systems do not control the fuselage attitude. This can result in the fuselage assuming an attitude controlled by momentum and tail rotor thrust that causes the tail boom to intersect the main rotor tip-path plane or result in the blade roots contacting the main rotor drive shaft, causing the blades to separate from the hub (mast bumping).

In the 2020s Robinson developed a new tail empennage for the R66 to reduce the chance of this type of accident. Two university studies of the Robinson main rotor, one by Georgia Tech and the other the University of Maryland, did not find the rotor design to be more susceptible in low-g conditions than other teetering designs, and this fit with Robinson's ongoing study of its design. Nevertheless, Robinson in the 2020s came up with new empennage to increase high speed roll stability, and this was approved by the FAA in 2023. Robinson hopes to bring this redesign to its other models, although low-g maneuvers remain forbidden. Low-g maneuvers are prohibited in Robinson designs even for demonstrations.

An example of accident attributed to low-g conditions, happened in Australia in 2020, when a R44 entered low-g conditions while flying through valleys, this led to extreme teetering and an ensuing break up of the aircraft.

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Fixed-wing aircraft

Low- g conditions can also affect fixed-wing aircraft in some instances, mainly by disrupting the airflow over the wings, making them difficult or impossible to control via the aerodynamic surfaces.

The controllability of an airplane by the control surfaces only depends on airspeed. So, if one keeps airspeed, control is retained. Usually the controllability is increased, because there is no need to produce lift. 0  g forces are a minimal problem for fixed wing aircraft, but there are exceptions, including, but not limited to, airplanes with gravity-fed fuel systems.

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Use in space agencies

To simulate 0- g conditions some space agencies uses a modified passenger aircraft to simulate a low- g condition. The ESA uses an Airbus A300, for example. NASA has the Vomit Comet. One upside down parabola simulates 0 g for about 25 s.

Categories: Aerodynamics, Gravity, Aviation Risks, Spaceflight Concepts

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