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Low-g condition is a phase of aerodynamic flight where the airframe is temporarily unloaded. The pilot—and the airframe—feel temporarily "weightless" 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.

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  • قوة تسارع منخفضة (ar)
  • Low-g condition (en)
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  • قوة تسارع منخفضة أو (بالإنجليزية: low-g)‏ هي مرحلة ايروديناميكية الطيران بحيث يكون الطيار وهيكل الطائرة منعدمي الوزن بشكل مؤقت، بسبب أن الطائرة تكون بحالة سقوط حر أو تباطؤ عمودي عند قمة الصعود. وقد تحدث بشكل أفقي عند المناورات الالتفاف. وقد يكون لها تأثير مدمر للطائرة، خصوصا لدى المروحيات، فهيكل البعض منها يحتاج أن يكون مقدار حملها لاصفري وبشكل دائم. (ar)
  • Low-g condition is a phase of aerodynamic flight where the airframe is temporarily unloaded. The pilot—and the airframe—feel temporarily "weightless" 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. (en)
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  • قوة تسارع منخفضة أو (بالإنجليزية: low-g)‏ هي مرحلة ايروديناميكية الطيران بحيث يكون الطيار وهيكل الطائرة منعدمي الوزن بشكل مؤقت، بسبب أن الطائرة تكون بحالة سقوط حر أو تباطؤ عمودي عند قمة الصعود. وقد تحدث بشكل أفقي عند المناورات الالتفاف. وقد يكون لها تأثير مدمر للطائرة، خصوصا لدى المروحيات، فهيكل البعض منها يحتاج أن يكون مقدار حملها لاصفري وبشكل دائم. (ar)
  • Low-g condition is a phase of aerodynamic flight where the airframe is temporarily unloaded. The pilot—and the airframe—feel temporarily "weightless" 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. (en)
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