• 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-1637

Effect of preignition on cylinder temperatures, pressures, power output, and piston failures

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1948

Abstract: An investigation using a cylinder of a V-type liquid-cooled engine was conducted to observe the behavior of the cylinder when operated under preignition conditions. The effects of the following variables were investigated: fuel-air ratio, power output, aromatic content of fuel, engine speed, mixture temperature, and preignition source. The power outputs at which preignition would cause complete piston failure for the selected engine operating conditions and the types of failure encountered when using various values of clearance between the piston and the cylinder barrel were determined.
URI: http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/190658
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (1.264Mb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NACA-TN-1637

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:07:43Z
date available2017-09-04T18:07:43Z
date copyright01/01/1948
date issued1948
identifier otherGPRTYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/190658
description abstractAn investigation using a cylinder of a V-type liquid-cooled engine was conducted to observe the behavior of the cylinder when operated under preignition conditions. The effects of the following variables were investigated: fuel-air ratio, power output, aromatic content of fuel, engine speed, mixture temperature, and preignition source. The power outputs at which preignition would cause complete piston failure for the selected engine operating conditions and the types of failure encountered when using various values of clearance between the piston and the cylinder barrel were determined.
languageEnglish
titleNACA-TN-1637num
titleEffect of preignition on cylinder temperatures, pressures, power output, and piston failuresen
typestandard
page41
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1948
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