This article explains how propeller's thrust is measured and modeled in a laboratory setting. It covers static thrust test methodology, the relationship between RPM and thrust force, and thrust coefficient modeling. A step-by-step experiment procedure and MATLAB implementation of the T = kω² thrust model are included.

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ITU Science Park, ARI4 Building
No: B204 Maslak 34469
Istanbul Turkey
+90 212 807 04 56
info@acrome.net




















