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ROSSINI SIGNED

Radial cOmpresSor Surge INception Investigation

Total Cost €

0

EC-Contrib. €

0

Partnership

0

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 ROSSINI project word cloud

Explore the words cloud of the ROSSINI project. It provides you a very rough idea of what is the project "ROSSINI" about.

models    piv    reference    relies    rotating    flow    instabilities    scenario    itself    modeling    aero    prerequisite    premature    ideally    start    investigations    sufficiently    diffuser    compressor    loads    orbit    data    impeller    separation    statement    resolved    pressure    predict    inception    diffusers    industrial    computational    experimentally    limited    mostly    aging    physical    induce    onset    stages    behavior    fatigue    damped    centrifugal    nonetheless    numerically    off    forth    academic    time    experimental    effort    hazardous    rotational    devoted    localized    first    quality    configuration    unsteady    oscillations    array    self    underlying    kulite    frequently    entire    phenomena    stage    elastic    operated    physics    nowadays    theoretical    effect    rotor    excited    margins    harmonic    speeds    safe    ultimate    vaneless    surge    stall    predicting    restricted    cells    put    sub    reported    outside    validation   

Project "ROSSINI" data sheet

The following table provides information about the project.

Coordinator
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV 

Organization address
address: Linder Hoehe
city: KOELN
postcode: 51147
website: www.dlr.de

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Germany [DE]
 Project website https://www.dlr.de/at/rossini
 Total cost 1˙102˙458 €
 EC max contribution 1˙102˙458 € (100%)
 Programme 1. H2020-EU.3.4.5.6. (ITD Systems)
 Code Call H2020-CS2-CFP02-2015-01
 Funding Scheme CS2-IA
 Starting year 2016
 Duration (year-month-day) from 2016-10-01   to  2021-03-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DE (KOELN) coordinator 747˙375.00
2    STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM NL (AMSTERDAM) participant 355˙083.00

Map

 Project objective

Centrifugal compressor stages using vaneless diffusers are known to have a wide operating range. However, when operated outside of this range, instabilities have been reported to commonly develop in the impeller (rotor) or diffuser or both. The unsteady flow phenomena are believed to start from a localized flow separation (stall) that frequently will orbit within the stage at sub-harmonic rotational speeds (rotating stall). If not damped sufficiently the stall cells will eventually develop into more hazardous self-excited pressure oscillations within the entire compressor stage leading to surge phenomena that can induce high aero-elastic loads on the rotor itself leading to premature aging (fatigue) or ultimate failure of the stage. Predicting of the onset of the instabilities is a prerequisite to maintain compressor operating within safe operating margins. Nonetheless the physical understanding and associated modeling of the stall and surge inception is rather limited and mostly restricted to cause-and-effect investigations. With improved computational models being available nowadays more in-depth investigations of the underlying flow physics have become possible, but relies on high quality experimental data for validation. Following the statement of work put forth in the call for proposal, the first objective of the proposed project is to determine a surge inception scenario for a given academic as well as industrial reference case of centrifugal compressor using vaneless diffuser. Within the proposed project the off-design behavior of each compressor configuration will be investigated both numerically and experimentally, involving time-resolved Kulite array and PIV measurements. Based on this data and on existing theoretical analysis procedures, the second major effort of the present study is devoted to define low-order methodologies that ideally predict the onset of instabilities.

 Publications

year authors and title journal last update
List of publications.
2017 Jonas ROSEMEIER
Numerische Analyse eines Radialverdichters mit Spiralgehäuse und unbeschaufeltem Diffusor
published pages: all, ISSN: , DOI:
Master Thesis (DLR-IB-AT-KP-2017-71) 2020-02-27
2017 Jonas ROSEMEIER
Numerical Analysis of a Centrifugal Compressor Including a Vaneless Diffuser and a Volute
published pages: , ISSN: , DOI:
ODAS 2017 17th ONERA-DLR Aerospace Sympos 2020-02-27

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