Zobrazeno 1 - 10
of 48
pro vyhledávání: '"H. E. Gallus"'
Publikováno v:
Journal of Turbomachinery. 125:173-182
The interaction between impeller and diffuser is considered to have strong influence on the flow in highly loaded centrifugal compressors. However, the knowledge about this influence is still not satisfying. This two-part paper presents an experiment
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::731b894e0492ed607c6ae91a2fe8a24e
https://doi.org/10.1115/1.1516814
https://doi.org/10.1115/1.1516814
Publikováno v:
MTZ - Motortechnische Zeitschrift. 61:508-514
Auf dem Gebiet der mehrstufigen Axialverdichter werden fur die Steigerung der Wirkungsgrade und Vergroserung der Betriebsbereiche grose Anstrengungen unternommen. Um dazu alle relevanten Aspekte der komplexen viskosen und instationaren Stromungsverha
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b8cf0fc09791e271e38a11b910a8486a
https://doi.org/10.1007/bf03226590
https://doi.org/10.1007/bf03226590
Publikováno v:
Journal of Propulsion and Power. 16:327-335
Anew three-dimensionalNavier–Stokesmethod for the analysisof the unsteady ow inmultiple turbomachinery blade rows is presented. To take into account turbulent effects, a low-Reynolds-numberk–2model is used. Smooth wave propagationaccross the s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a05c008877cc344200e807bb337b0dab
https://doi.org/10.2514/2.5573
https://doi.org/10.2514/2.5573
Publikováno v:
Journal of Turbomachinery. 121:763-771
The behaviour of vaned radial diffusers is generally considered to be due to the flow phenomena in the vaneless and the semi-vaned space in the diffuser inlet region. Even considering unsteady aspects, the adjacent diffuser channel is regarded as les
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d0147a580562a8ad625fc980089aac40
https://doi.org/10.1115/1.2836730
https://doi.org/10.1115/1.2836730
Autor:
H. E. Gallus, Frank Mildner
Publikováno v:
Journal of Turbomachinery. 120:744-752
The subject of this paper is a numerical method for the calculation of the transonic flow field of multistage turbines, taking high coolant flow into account. To reduce the processing time, a throughflow method based on the principles of Wu is used f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d2a9139471a6f61b332cd4857e154721
https://doi.org/10.1115/1.2841785
https://doi.org/10.1115/1.2841785
Autor:
H. E. Gallus, C. Poensgen
Publikováno v:
Journal of Turbomachinery. 118:189-196
This paper describes the results on an experimental investigation of rotating stall flow inside a single-stage axial flow compressor. Tests were carried out in two steps. First, measurements were taken to investigate the transition process into rotat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce4d196bb11105d583f5d630fa9b9ec2
https://doi.org/10.1115/1.2836625
https://doi.org/10.1115/1.2836625
Autor:
H. E. Gallus, H. Hönen
Publikováno v:
Journal of Turbomachinery. 117:81-86
The unsteady flow in a single-stage axial flow compressor at different operating conditions has been investigated with hot-wire and hot-film probes to find out the influence of the aerodynamic compressor load on the periodic fluctuations. These resul
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::87fbca3cf86fdece4a4bc871707b9147
https://doi.org/10.1115/1.2835645
https://doi.org/10.1115/1.2835645
Publikováno v:
Journal of Turbomachinery. 115:565-572
In consideration of further jet-engine developments required by applications for supersonic travel aircraft, airbreathing propulsion of space vehicles or only the improvement of conventional high performance turbo engines, highly loaded supersonic co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a31462cb180181ed2f39a0af35d9f992
https://doi.org/10.1115/1.2929291
https://doi.org/10.1115/1.2929291
Autor:
H. E. Gallus, Hannes Benetschik
Publikováno v:
Journal of Propulsion and Power. 8:403-409
This article presents a numerical algorithm for calculating inviscid and viscous flows in transonic and super- sonic turbomachinery cascades. Of particular interest is the prediction of shock-induced boundary-layer sep- aration and the comparison wit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a8aa65d737626a879536fb135b4075be
https://doi.org/10.2514/3.23492
https://doi.org/10.2514/3.23492
Publikováno v:
Journal of Turbomachinery. 113:198-206
A detailed experimental and numerical investigation was carried out to examine the three-dimensional flow field, secondary flows and vortex motion in an annular compressor cascade. Various flow visualizations near the blade surface and endwalls, wall
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c79ee060d79956e050d7da15b4834cc1
https://doi.org/10.1115/1.2929083
https://doi.org/10.1115/1.2929083