Experimental investigation of a radial turboshaft engine intake

Fabian Fuchs, Christian Schäffer, Volker Gümmer

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

1 Scopus citations

Abstract

The present publication gives an introduction to an experimental approach of investigating the aerodynamic behavior of the intake used for turboshaft engines. All the work is carried out in the chair’s laboratories, a blower and a test stand for turboshaft engines for helicopter propulsion. This paper gives a complete test facility description followed by primary measurement results. The measurements on the intake are taken with free inflow as well as with distorted inflow, which is split in temperature and total pressure distortions. The results show the impact of the inlet distortions on the flow pattern in the AIP.

Original languageEnglish
Title of host publication2018 Joint Propulsion Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105708
DOIs
StatePublished - 2018
Event54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018 - Cincinnati, United States
Duration: 9 Jul 201811 Jul 2018

Publication series

Name2018 Joint Propulsion Conference

Conference

Conference54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018
Country/TerritoryUnited States
CityCincinnati
Period9/07/1811/07/18

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