• 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

NASA-TM-X-72697

Low-speed aerodynamic characteristics of a 13-percent-thick airfoil section designed for general aviation applications

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1975

Abstract: Wind-tunnel tests were conducted to determine the low-speed section characteristics of a 13 percent-thick airfoil designed for general aviation applications. The results were compared with NACA 12 percent-thick sections and with the 17 percent-thick NASA airfoil. The tests were conducted ovar a Mach number range from 0.10 to 0.35. Chord Reynolds numbers varied from about 2,000,000 to 9,000,000.
URI: https://yse.yabesh.ir/std/handle/yse/32235
Subject: AERODYNAMIC
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (1.927Mb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NASA-TM-X-72697

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:30:47Z
date available2017-09-04T15:30:47Z
date copyright01/01/1975
date issued1975
identifier otherAWTKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/32235
description abstractWind-tunnel tests were conducted to determine the low-speed section characteristics of a 13 percent-thick airfoil designed for general aviation applications. The results were compared with NACA 12 percent-thick sections and with the 17 percent-thick NASA airfoil. The tests were conducted ovar a Mach number range from 0.10 to 0.35. Chord Reynolds numbers varied from about 2,000,000 to 9,000,000.
languageEnglish
titleNASA-TM-X-72697num
titleLow-speed aerodynamic characteristics of a 13-percent-thick airfoil section designed for general aviation applicationsen
typestandard
page58
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1975
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsAIRFOIL
subject keywordsAVIATION
subject keywordsCHARACTERISTICS
subject keywordsCOEFFICIENTS
subject keywordsGENERAL
subject keywordsLOW
subject keywordsMODELS
subject keywordsNUMBER
subject keywordsPROFILES
subject keywordsREYNOLDS
subject keywordsSPEED
subject keywordsSTABILITY
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
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