IMPACT: Experimental and Numerical Ice Shapes on Swept-Wing Models with Straight and Undulated Leading Edges
AIAA AVIATION FORUM AND ASCEND 2024
01.01.2024
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Stall Inception in Single-Stage, Transonic Compressors with Straight and Swept Leading Edges
Online Contents | 1995
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