Show simple item record

Summary of section data on trailing-edge high-lift devices

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:43:04Z
date available2017-09-04T18:43:04Z
date copyright01/01/1949
date issued1949
identifier otherKAXUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/224476
description abstractA summary has been made of available data on the characteristics of airfoil sections with trailing-edge high-lift devices. Data for plain, split, and slotted flaps are collected and analyzed. The effects of each of the variables involved in the design of the various types of flap are examined and, in cases where sufficient data are given, optimum configurations are deduced. Wherever possible, the effects of airfoil section, Reynolds number, and leading-edge roughness are shown. For single and double slotted flaps, where a large amount of unrelated data are available, maximum lift coefficients of many configurations are presented in tables.
languageEnglish
titleNACA-TR-938num
titleSummary of section data on trailing-edge high-lift devicesen
typestandard
page36
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1949
contenttypefulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record