Supercooled Large Droplets impingement simulation of 3-element airfoils

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

6 Scopus citations

Abstract

Under the condition of supercooled large droplets (SLD), droplets breakup, splashing and bouncing should be considered. A droplet re-impingement model is applied to better study SLD impingement, and the Mcdonnell Douglas Aerospace (MDA) 3-element airfoils are simulated. Compared with normal model, impingement limits are minished slightly, local water collection efficiency decreases in some degree, and LWC in different areas of flow space vary. The simulated results are in better accordance with wind tunnel experiments, which indicates that the model that considering splashing and bouncing is more accurate and closer to reality when simulating SLD impingement.

Original languageEnglish
Title of host publicationProceedings of 2017 8th International Conference on Mechanical and Intelligent Manufacturing Technologies, ICMIMT 2017
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages225-229
Number of pages5
ISBN (Electronic)9781538603772
DOIs
StatePublished - 2 May 2017
Event8th International Conference on Mechanical and Intelligent Manufacturing Technologies, ICMIMT 2017 - Cape Town, South Africa
Duration: 3 Feb 20176 Feb 2017

Publication series

NameProceedings of 2017 8th International Conference on Mechanical and Intelligent Manufacturing Technologies, ICMIMT 2017

Conference

Conference8th International Conference on Mechanical and Intelligent Manufacturing Technologies, ICMIMT 2017
Country/TerritorySouth Africa
CityCape Town
Period3/02/176/02/17

Keywords

  • Droplets breakup
  • Droplets impingement
  • SLD
  • Splashing and bouncing

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