Zobrazeno 1 - 5
of 5
pro vyhledávání: '"W. D. E. Allan"'
Publikováno v:
Volume 2A: Turbomachinery.
A series of experiments has been undertaken on a swept cylinder in cross-flow in the 2m2 open-jet wind-tunnel at Durham University, at a nominal Reynolds Number of 500,000. Boundary layer instability, leading to transition has been attributed to curi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dabf497cc08d6d81d256c4c9cc909ff0
https://doi.org/10.1115/gt2015-43847
https://doi.org/10.1115/gt2015-43847
Publikováno v:
Volume 2A: Turbomachinery.
Even for the ostensibly two-dimensional flow through cascades of blades, many details of the flow physics are neither well-understood nor well-predicted. Gaps in knowledge are identified that cover entire blade and nozzle vane surfaces from leading e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5cfaa413985df2b46b10b78fdb8e6148
https://doi.org/10.1115/gt2015-44130
https://doi.org/10.1115/gt2015-44130
Autor:
W. D. E. Allan, J. Ilott
Publikováno v:
Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation.
In addition to their small size, miniature silicon pressure transducers offer wide-band frequency response. Taking advantage of the high-frequency response of these pressure transducers within an electrically noisy environment requires high bandwidth
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::367ff46409ea79bf7e4502d646201f3f
https://doi.org/10.1115/gt2012-70036
https://doi.org/10.1115/gt2012-70036
Publikováno v:
Volume 7: Turbomachinery, Parts A, B, and C.
This paper addresses the issue of aerodynamic consequences of variations in airfoil profile. An analysis of new and repaired airfoils was used to synthesize profiles representative of specific repair types. Five variations of a reference new low pres
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aa3411fdff0cd917255e4af215aebee6
https://doi.org/10.1115/gt2011-46558
https://doi.org/10.1115/gt2011-46558
Autor:
W. D. E. Allan, L. G. N. Bennett
Publikováno v:
Volume 7: Turbomachinery, Parts A and B.
Rotating stall is an internal aerodynamic disturbance that limits the performance and operating life of a compressor. It has been studied with the aim of developing techniques for its prediction and prevention. To further the understanding of rotatin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::80ce86512fd39bd75238de82f1891daa
https://doi.org/10.1115/gt2009-59420
https://doi.org/10.1115/gt2009-59420