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A transonic propeller of triangular plan form

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:11:49Z
date available2017-09-04T16:11:49Z
date copyright01/01/1947
date issued1947
identifier otherBJLUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/75001
description abstractAn isosceles triangle twisted into a screw surface about its axis is proposed as a propeller for transonic flight speeds. The purpose is to attain the drag reduction associated with large sweepback in a structurally practicable configuration. A mathematical theory for such a propeller is presented. Calculations taking account of wave and skin-friction drag indicate a net efficiency of the order of 80 percent at Mach number 1.1. A 12-foot propeller is estimated to be able to absorb 18,500 brake horsepower at 840 miles per hour at sea level.
languageEnglish
titleNACA-TN-1303num
titleA transonic propeller of triangular plan formen
typestandard
page42
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1947
contenttypefulltext


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