Pages that link to "Item:Q1404585"
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The following pages link to Study on the propagation of inlet flow distortion in axial compressor using an integral method (Q1404585):
Displaying 3 items.
- Stall prediction of in-flight compressor due to flamming of refueling leakage near inlet (Q1420031) (← links)
- Preliminary study to raise axial flow compressors up to the context-awareness standards (Q2853529) (← links)
- Numerical Parametric Study of Inlet Distortion Propagation in Compressor Using Integral Approach with Taguchi Method (Q6586200) (← links)
