Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Reinhard Mönig"'
Autor:
Reinhard Mönig, Ulrich Waltke
Publikováno v:
Stationäre Gasturbinen ISBN: 9783662561331
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a6824dc702fe023490235df910fab716
https://doi.org/10.1007/978-3-662-56134-8_7
https://doi.org/10.1007/978-3-662-56134-8_7
Publikováno v:
Journal of Turbomachinery. 123:558-567
During the last few decades extremely powerful Quasi-three-dimensional (3D) codes and fully 3D Navier-Stokes solvers have been developed and successfully utilized in the design process and optimization of multistage axial-flow compressors. However, m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a599fe973338b24c7fc9769dfb4ca4c1
https://doi.org/10.1115/1.1370167
https://doi.org/10.1115/1.1370167
Publikováno v:
Journal of Turbomachinery. 122:397-405
A new family of subsonic compressor airfoils, which are characterized by low losses and wide operating ranges, has been designed for use in heavy-duty gas turbines. In particular the influence of the higher airfoil Reynolds numbers compared to aeroen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f3f8786ed030996f88e68c62ce1908e0
https://doi.org/10.1115/1.1302296
https://doi.org/10.1115/1.1302296
Publikováno v:
Journal of Turbomachinery. 122:406-414
In Part I of this paper a family of numerically optimized subsonic compressor airfoils for heavy-duty gas turbines, covering a wide range of flow properties, is presented. The objective of the optimization was to create profiles with a wide low loss
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13141585d99c1d986c75cb42cf246a61
https://doi.org/10.1115/1.1302321
https://doi.org/10.1115/1.1302321
Publikováno v:
Volume 6A: Turbomachinery.
The application of casing treatments (CT) is an effective measure to increase the stable operating range of modern aero engine or gas turbine compressors. As the development and design process of optimized CT geometries is primarily based on numerica
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::71274597b60a1b1f1b21ac6f6031033c
https://doi.org/10.1115/gt2013-94006
https://doi.org/10.1115/gt2013-94006
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
Publikováno v:
Journal of Turbomachinery. 133
A single-stage transonic axial compressor was equipped with a casing treatment (CT), consisting of 3.5 axial slots per rotor pitch in order to investigate the predicted extension of the stall margin characteristics both numerically and experimentally
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bc06d1c94fb610579202051e446d2901
https://doi.org/10.1115/1.4000489
https://doi.org/10.1115/1.4000489
This contribution is aimed at summarizing the effort taken to apply stereoscopic PIV (SPIV) measurements in the tip clearance of a transonic compressor rotor equipped with a casing treatment. A light sheet probe was placed downstream of the stator an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::06caa8be30e7c129c9825657998790f7
https://elib.dlr.de/64651/
https://elib.dlr.de/64651/
Autor:
Reinhard Mönig, Ulrich Waltke
Publikováno v:
Stationäre Gasturbinen ISBN: 9783540927877
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eec0004c75e4b4c34981c94626bad9c3
https://doi.org/10.1007/978-3-540-92788-4_7
https://doi.org/10.1007/978-3-540-92788-4_7
Publikováno v:
Volume 6: Turbomachinery, Parts A, B, and C.
In combination with a multi-objective 3D optimization strategy, a linked CFD-solver is presented in this paper, combining 3D-Reynolds-averaged-Navier-Stokes and an inviscid throughflow method. It enables the adjustment of the 3D boundary conditions f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f1571d7a858c9af4ec3a02a77929d7d0
https://doi.org/10.1115/gt2008-51131
https://doi.org/10.1115/gt2008-51131