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NASA NTRS ยท 19930094591

The Source of Propeller Noise

Abstract

A two blade propeller of 40 cm diameter and zero pitch was explored for its noise development; it could be whirled up to 17,000 rpm - i.e., a tip speed of 355 meters/second. To obtain the power loss N(sub m) of the propeller for comparison with the produced acoustical power N(sub A) the engine performance characteristics were measured with and without propeller. The result is the sought-for relation c, that is, curve c' after correction with the engine efficiency.

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BibTeXRIS

Ernsthausen, W. 1937-05-01. The Source of Propeller Noise. https://ntrs.nasa.gov/citations/19930094591

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