Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Michael Benner"'
Publikováno v:
8th AIAA Atmospheric and Space Environments Conference.
Autor:
Alfred Rieckers, Michael Benner
Publikováno v:
Zeitschrift für Naturforschung A. 60:343-365
For a class of Bardeen-Cooper-Schrieffer (BCS)-models, with complex, weakly momentum dependent interaction coefficients, the representation dependent effective Hamiltonians and their spectra are reconsidered in order to obtain a consistent physical p
Publikováno v:
Journal of Turbomachinery. 128:281-291
A new empirical prediction method for design and off-design secondary losses in turbines has been developed. The empirical prediction method is based on a new loss breakdown scheme, and as discussed in Part I, the secondary loss definition in this ne
Publikováno v:
Volume 2A: Turbomachinery.
Three-dimensional corner stall is one of the most important factors limiting compressor performance. This paper presents a complementary experimental and computational study of corner stall in a highly-loaded compressor cascade subjected to three inl
This paper presents an experimental investigation of the flow mechanisms in an aggressive interturbine transition duct with and without low-profile vortex generators flow control. The interturbine duct had an area ratio of 1.53 and a mean rise angle
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6fa3cf43ae667019a4735f6dfcd0e3a4
https://doi.org/10.1115/1.4027656
https://doi.org/10.1115/1.4027656
This paper presents the experimental investigation of the flow in an aggressive inter-turbine duct (AITD). The goal is to improve the understanding of the flow mechanisms within the AITD and of the underlying physics of lowprofile vortex generators (
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2bd361e98c864f28cb9b561cc33b97b2
https://nrc-publications.canada.ca/eng/view/object/?id=3307890f-9e98-4a8d-975e-159d3748d3d2
https://nrc-publications.canada.ca/eng/view/object/?id=3307890f-9e98-4a8d-975e-159d3748d3d2
Publikováno v:
Volume 7: Fluid Flow, Heat Transfer and Thermal Systems, Parts A and B.
The inter-turbine transition duct (ITD) between the high-pressure (HP) and low-pressure (LP) turbines of a gas turbine has the potential for significant length reduction and therefore engine weight reduction and/or aerodynamic performance improvement
Publikováno v:
Volume 7: Fluid Flow, Heat Transfer and Thermal Systems, Parts A and B.
To reduce the harmful effects of aviation on the environment, aircraft gas turbine manufacturers continue to focus on producing engines with lower specific fuel consumption and weight. To address the engine weight challenges, R&D efforts continue to
ASME Turbo Expo 2004, June 14-17, 2004., Vienna, Austria
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Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3914706c99367839894ef90a2c467a84
https://nrc-publications.canada.ca/eng/view/object/?id=13a0a0d2-984f-47c3-becc-f8274062de84
https://nrc-publications.canada.ca/eng/view/object/?id=13a0a0d2-984f-47c3-becc-f8274062de84