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Axi-symmetric stall, more commonly known as compressor surge; or pressure surge, is a complete breakdown in compression resulting in a reversal of flow and the violent expulsion of previously compressed air out through the engine intake, due to the compressor's inability to continue working against the already-compressed air behind it. The ...
While fully developed compressor surge is axisymmetric, its initial phase is not necessarily axisymmetric. Actually, severe damage of compressor surge is often related to very large transverse loads on blades and casing in its initial transient. [7] A chain reaction of compressor surge is the flameout of a jet engine. Due to a lack of air ...
A compressor surge is a disruption of the airflow through a gas turbine jet engine that can be caused by engine deterioration, a crosswind over the engine's inlet, ice accumulation around the engine inlet, ingestion of foreign material, or an internal component failure such as a broken blade. While this situation can be alarming, the engine may ...
The cause for me to make these suggestions is my interest in referencing a "primary article" to replace the Surge/surge line/stall/stall line discussion in "Centrifugal compressor". The suggestions I would like to make involves everyone, Wikipedia, contributors to Compressor stall, and contributors to Surge in compressors.
At speeds below the intake starting speed, or on aircraft with external compression intakes, engine surge or compressor stall can cause a hammershock. Above the intake starting speed, unstarts can cause stalls depending on the intake systems design complexity. [21] Hammershocks have caused damage to intakes.
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There was some years ago a PBS NOVA show suggesting that 1973_Paris_Air_Show_Tu-144_crash was due to (as well as I remember now) compressor stall or surge during an evasive maneuver. That the way to recover is a high-speed dive to get enough air though the engine, but that they hit the ground before recovering.
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