• 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-ARR-L4I11 REV F

Wind-Tunnel Investigation of Control-Surface Characteristics XX - Plain and Balanced Flaps on an NACA 0009 Rectangular Semispan Tail Surface

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1944

Abstract: Correlation is established between aerodynamic characteristics of control surfaces in two-dimensional and three-dimensional flow. Slope of lift curve was affected little by overhang and balance-nose shape, but increased by sealing flap-nose gap. Effectiveness of balancing tab was same for sealed plain flap and unsealed overhang flap. Changes in hinge-moment coefficient were diminished by sealing gap. Values measured by three-dimensional flow disagreed with two-dimensional flow values until aspect ratio corrections were made.
URI: http://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/212516
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (1.647Mb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NACA-ARR-L4I11 REV F

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:30:16Z
date available2017-09-04T18:30:16Z
date copyright01/01/1944
date issued1944
identifier otherIVUYYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/212516
description abstractCorrelation is established between aerodynamic characteristics of control surfaces in two-dimensional and three-dimensional flow. Slope of lift curve was affected little by overhang and balance-nose shape, but increased by sealing flap-nose gap. Effectiveness of balancing tab was same for sealed plain flap and unsealed overhang flap. Changes in hinge-moment coefficient were diminished by sealing gap. Values measured by three-dimensional flow disagreed with two-dimensional flow values until aspect ratio corrections were made.
languageEnglish
titleNACA-ARR-L4I11 REV Fnum
titleWind-Tunnel Investigation of Control-Surface Characteristics XX - Plain and Balanced Flaps on an NACA 0009 Rectangular Semispan Tail Surfaceen
typestandard
page58
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1944
contenttypefulltext
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