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- Low-g_condition abstract "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.".
- Low-g_condition wikiPageID "3512082".
- Low-g_condition wikiPageRevisionID "598122746".
- Low-g_condition hasPhotoCollection Low-g_condition.
- Low-g_condition subject Category:Aerodynamics.
- Low-g_condition subject Category:Aviation_risks.
- Low-g_condition subject Category:Gravitation.
- Low-g_condition subject Category:Spaceflight_concepts.
- Low-g_condition type AviationRisks.
- Low-g_condition type CausalAgent100007347.
- Low-g_condition type Danger114541044.
- Low-g_condition type Hazard114541852.
- Low-g_condition type PhysicalEntity100001930.
- Low-g_condition comment "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.".
- Low-g_condition label "Low-g condition".
- Low-g_condition label "قوة تسارع منخفضة".
- Low-g_condition sameAs m.09hl44.
- Low-g_condition sameAs Q6692755.
- Low-g_condition sameAs Q6692755.
- Low-g_condition sameAs Low-g_condition.
- Low-g_condition wasDerivedFrom Low-g_condition?oldid=598122746.
- Low-g_condition isPrimaryTopicOf Low-g_condition.