Active flow control of complex configurations

Artur Minasyan, David Sidilkover, Avi Seifert

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

Abstract

A flow analysis and boundary layer control were applied to an inlet shape design that is efficient from the external aerodynamic point of view, but due to its short and high offset suffers from internal flow separations and significant engine face distortions. For simplicity, low Reynolds number and low (practically incompressible) Mach number experiments and simulations were performed on an equivalent 2D geometry. Qualitative agreement was found between experiments and simulations. Preliminary efforts to control this complex flow are presented and tested both by experiments and simulations.

Original languageEnglish
Title of host publication54th Israel Annual Conference on Aerospace Sciences 2014
PublisherTechnion Israel Institute of Technology
Pages395-410
Number of pages16
ISBN (Print)9781632662651
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
Volume1

Conference

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

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