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Propeller rotation noise due to torque and thrust

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:59:33Z
date available2017-09-04T17:59:33Z
date copyright01/01/1940
date issued1940
identifier otherFUONEEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/182682
description abstractSound pressure of the first four harmonics of rotation from a full-scale two-blade propeller were measured and are compared with values calculated from theory. The comparison is made (1) for the space distribution with constant tip speed and (2) for fixed space angles with variable tip speed. A relation for rotation noise from an element of radius developed by Gutin is given showing the effect of number of blades on the rotation noise.
languageEnglish
titleNACA-TN-747num
titlePropeller rotation noise due to torque and thrusten
typestandard
page19
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1940
contenttypefulltext


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