Aerodynamic Performance of an Active flow Control Configuration Using Unstructured-Grid RANS
39th, Aerospace sciences meeting ; 2001 ; Reno, NV
01.01.2001
ALL
Paper nos AIAA-2001-0003 to AIAA-2001-0660 with gaps
Aufsatz (Konferenz)
Englisch
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RANS Computation of Tip Clearance Flow in a Compressor Cascade Using an Unstructured Grid
British Library Conference Proceedings | 2001
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