• 0
    • ارسال درخواست
    • حذف همه
    • Industrial Standards
    • Defence Standards
  • درباره ما
  • درخواست موردی
  • فهرست استانداردها
    • Industrial Standards
    • Defence Standards
  • راهنما
  • Login
  • لیست خرید شما 0
    • ارسال درخواست
    • حذف همه
View Item 
  •   YSE
  • Defence Standards
  • NASA - National Aeronautics and Space Administration (NASA)
  • View Item
  •   YSE
  • Defence Standards
  • NASA - National Aeronautics and Space Administration (NASA)
  • View Item
  • All Fields
  • Title(or Doc Num)
  • Organization
  • Year
  • Subject
Advanced Search
JavaScript is disabled for your browser. Some features of this site may not work without it.

Archive

NACA-TN-1473

High-speed wind-tunnel investigation of high lift and aileron-control characteristics of an NACA 65-210 semi-span wing

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1947

Abstract: A high-speed wind-tunnel investigation was made of the aerodynamic characteristics at various Mach numbers of an NACA 65-210 semispan wing variously equipped with a 25-percent chord full-span slotted flap and 38-percent-semispan 20-percent-chord straight-saided aileron.
With the full-span flap retracted at a Mach number of 0.13, a maximum lift coefficient of 0.93 was obtained; and with the flap deflected 45°, a maximum lift coefficient of 1.87 was obtained.
URI: https://yse.yabesh.ir/std/handle/yse/83423
Subject: AILERONS
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (842.8Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NACA-TN-1473

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:19:57Z
date available2017-09-04T16:19:57Z
date copyright01/01/1947
date issued1947
identifier otherBLXSYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/83423
description abstractA high-speed wind-tunnel investigation was made of the aerodynamic characteristics at various Mach numbers of an NACA 65-210 semispan wing variously equipped with a 25-percent chord full-span slotted flap and 38-percent-semispan 20-percent-chord straight-saided aileron.
With the full-span flap retracted at a Mach number of 0.13, a maximum lift coefficient of 0.93 was obtained; and with the flap deflected 45°, a maximum lift coefficient of 1.87 was obtained.
languageEnglish
titleNACA-TN-1473num
titleHigh-speed wind-tunnel investigation of high lift and aileron-control characteristics of an NACA 65-210 semi-span wingen
typestandard
page33
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1947
contenttypefulltext
subject keywordsAILERONS
subject keywordsAIRFOILS
subject keywordsCARRIED
subject keywordsCHAR
subject keywordsDRAG
subject keywordsFLAPS
subject keywordsFULL
subject keywordsHIGH
subject keywordsHINGE
subject keywordsLMAL
subject keywordsLOW
subject keywordsMOMENTS
subject keywordsNACA
subject keywordsORDINATES
subject keywordsPARTIAL
subject keywordsROLLING
subject keywordsSLOTTED
subject keywordsSPAN
subject keywordsSPEED
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS
subject keywordsWORK
subject keywordsYAWING
DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian
 
DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian