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Liu , B. ; Tao , Y. ; Yu , X. Application of MCST methodto designthe blade leading edge in axial compressors
Rough airwill causecompressor stall despite the variable pitch stator blades on the fist stages of the compressor section
downstream airflow turbulencecausinghigh stresses in the 2nd stage axial compressor wheel blades
Banks Engineering ’s solution to this wasto createa compressor wheel that features staggered , angle - cut blades
These tighter clearancescan resultin compressor blade tips and turbine blade tips rubbing on the engine cases
an excessively small clearance results in high forces being required to turn the vane 12 , which can overstress the actuation hardware andcould ... preventactuation of the vane 12 ... leading to compressor stall
when airflow is lowcausingthe flow on the compressor blade suction side to separate
understanding of the fluid dynamics mechanismsleadto rotating stall in the axial flow low speed compressor stage
thermal growth rates of the compressor rotor and stator assemblies(passive) caused byexcessive compressor blade clearances in the HPC
This AD(passive) was prompted byThis AD
for high pressure ratio , report , July 10 , 1950designedfor high pressure ratio , report , July 10 , 1950
Commencement and development processes of unsteadiness(passive) caused byCommencement and development processes of unsteadiness
for high pressure ratio - Digital Library Effect of Mach number on over - all performance of single - stage axial - flow compressor designed for high pressuredesignedfor high pressure ratio - Digital Library Effect of Mach number on over - all performance of single - stage axial - flow compressor designed for high pressure
damage thereto(passive) caused bydamage thereto
surgecausessurge
to a relatively wider operating range and a better operabilityleadingto a relatively wider operating range and a better operability
the liquid water to evaporatecausingthe liquid water to evaporate