• 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-73566

Interim Prediction Method for Turbine Noise

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1976

Abstract: A turbine noise prediction method for interim use in the NASA Aircraft Noise Prediction Program is selected. The method predicts the level, directivity, and one-third octave band spectra of far field turbine noise as a function of engine parameters. The selection results from a review of turbine noise data and prediction methods available in the open literature. It is concluded that the state-of-the-art turbine noise prediction capability is primitive and that the selected method represents only a temporary interim approach. Recommendations are made on research requirements.
URI: http://yse.yabesh.ir/std/handle/yse/177655
Subject: AIRCRAFT ENGINES
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (870.7Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NASA-TM-X-73566

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:54:34Z
date available2017-09-04T17:54:34Z
date copyright01/01/1976
date issued1976
identifier otherFHLNGEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/177655
description abstractA turbine noise prediction method for interim use in the NASA Aircraft Noise Prediction Program is selected. The method predicts the level, directivity, and one-third octave band spectra of far field turbine noise as a function of engine parameters. The selection results from a review of turbine noise data and prediction methods available in the open literature. It is concluded that the state-of-the-art turbine noise prediction capability is primitive and that the selected method represents only a temporary interim approach. Recommendations are made on research requirements.
languageEnglish
titleNASA-TM-X-73566num
titleInterim Prediction Method for Turbine Noiseen
typestandard
page25
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1976
contenttypefulltext
subject keywordsAIRCRAFT ENGINES
subject keywordsAIRCRAFT NOISE
subject keywordsDIRECTIVITY
subject keywordsENGINE NOISE
subject keywordsNOISE INTENSITY
subject keywordsPREDICTION ANALYSIS TECHNIQUES
subject keywordsTECHNOLOGY ASSESSMENT
subject keywordsTURBINES
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