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NACA-TN-690

Resume of air-load data on slats and flaps

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1939

Abstract: A resume of the generally available test data regarding air loads on slats and flaps is presented and data attained up to the fall of 1938 are included. The data are given in the form of N.A.C.A. standard coefficients of air forces and moments on the lift-increasing device and, when available, the aerodynamic characteristics of the combined wing and high-lift device are included. Slats of the Handley Page type, fixed auxiliary airfoils, and flaps of several different types are covered.
URI: https://yse.yabesh.ir/std/handle/yse/14671
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    NACA-TN-690

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:15:39Z
date available2017-09-04T15:15:39Z
date copyright01/01/1939
date issued1939
identifier otherMGYIYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/14671
description abstractA resume of the generally available test data regarding air loads on slats and flaps is presented and data attained up to the fall of 1938 are included. The data are given in the form of N.A.C.A. standard coefficients of air forces and moments on the lift-increasing device and, when available, the aerodynamic characteristics of the combined wing and high-lift device are included. Slats of the Handley Page type, fixed auxiliary airfoils, and flaps of several different types are covered.
languageEnglish
titleNACA-TN-690num
titleResume of air-load data on slats and flapsen
typestandard
page38
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1939
contenttypefulltext
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DSpace software copyright © 2017-2020  DuraSpace
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