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NACA-TN-2335

A plan-form parameter for correlating certain aerodynamic characteristics of swept wings

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1951

Abstract: On the basis of approximate expressions for the lift-curve slope and the coefficient of damping in roll of swept wings at subsonic speeds, the finite-span effects on these aerodynamic characteristics are shown to be functions primarily of a plan-form parameter, which is the aspect ratio divided by the cosine of the sweep angle and by the ratio of the section lift-curve slope to 2π. The use of this parameter in presenting concisely and in correlating certain aerodynamic characteristics and the limitations attendant upon such use are discussed.
URI: http://yse.yabesh.ir/std/handle/yse/153255
Subject: ASPECT
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    NACA-TN-2335

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:30:12Z
date available2017-09-04T17:30:12Z
date copyright01/01/1951
date issued1951
identifier otherCUJUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/153255
description abstractOn the basis of approximate expressions for the lift-curve slope and the coefficient of damping in roll of swept wings at subsonic speeds, the finite-span effects on these aerodynamic characteristics are shown to be functions primarily of a plan-form parameter, which is the aspect ratio divided by the cosine of the sweep angle and by the ratio of the section lift-curve slope to 2π. The use of this parameter in presenting concisely and in correlating certain aerodynamic characteristics and the limitations attendant upon such use are discussed.
languageEnglish
titleNACA-TN-2335num
titleA plan-form parameter for correlating certain aerodynamic characteristics of swept wingsen
typestandard
page19
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1951
contenttypefulltext
subject keywordsASPECT
subject keywordsCHARACTERISTICS
subject keywordsDAMPING
subject keywordsRATIO
subject keywordsROLL
subject keywordsSWEPTBACK
subject keywordsSWEPTFORWARD
subject keywordsTHEORIES
subject keywordsWINGS
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DSpace software copyright © 2017-2020  DuraSpace
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