Aeroelastic CFD analysis of a rotating propeller

Yuval Levy, Daniella E. Raveh

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

Abstract

A new capability to conduct aeroelastic flow simulations coupled with 6 degrees of freedom motion has been added to the EZNSS flow solver. The new capabilities have been tested by simulating the flow about an elastic rotating propeller under low subsonic flow conditions. The results show that elasticity does have an effect on the thrust. In the current case the thrust is reduced.

Original languageEnglish
Title of host publication54th Israel Annual Conference on Aerospace Sciences 2014
Pages838-851
Number of pages14
StatePublished - 2014
Event54th Israel Annual Conference on Aerospace Sciences, IACAS 2014 - Tel-Aviv and Haifa, Israel
Duration: 19 Feb 201420 Feb 2014

Publication series

Name54th Israel Annual Conference on Aerospace Sciences 2014
Volume2

Conference

Conference54th Israel Annual Conference on Aerospace Sciences, IACAS 2014
Country/TerritoryIsrael
CityTel-Aviv and Haifa
Period19/02/1420/02/14

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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