• 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-RB-3L02

Proposal for a propeller side-force facto

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1943

Abstract: Knowledge of the side force on a propeller in yaw The fin effect - is useful in the design of tail surfaces, in the testing of powered. aircraft models, and I in formal. stability and control analyses. A side-force factor computed from the plan form and pitch distribution in shown to be a good index of the relative effectiveness, per blade, of a yawed propeller in developing side force. By the general use of side–force factors, existing charts of propeller side force may be simply extrapolated to" give Me side force on any specified propeller in any specified operating condition. The suggestion is made that propeller manufacturers and designers present the stale-force factor with the activity factor as a fundamental parameter for all blade designs and that reports of tests of powered models in wind tunnels include the side-force factor for the propeller used.
URI: http://yse.yabesh.ir/std/handle/yse/164032
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (350.3Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NACA-RB-3L02

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:41:06Z
date available2017-09-04T17:41:06Z
date copyright01/01/1943
date issued1943
identifier otherDWUYYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/164032
description abstractKnowledge of the side force on a propeller in yaw The fin effect - is useful in the design of tail surfaces, in the testing of powered. aircraft models, and I in formal. stability and control analyses. A side-force factor computed from the plan form and pitch distribution in shown to be a good index of the relative effectiveness, per blade, of a yawed propeller in developing side force. By the general use of side–force factors, existing charts of propeller side force may be simply extrapolated to" give Me side force on any specified propeller in any specified operating condition. The suggestion is made that propeller manufacturers and designers present the stale-force factor with the activity factor as a fundamental parameter for all blade designs and that reports of tests of powered models in wind tunnels include the side-force factor for the propeller used.
languageEnglish
titleNACA-RB-3L02num
titleProposal for a propeller side-force factoen
typestandard
page14
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1943
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