Zobrazeno 1 - 10
of 38
pro vyhledávání: '"multi-hole probe"'
Publikováno v:
Sensors, Vol 22, Iss 6, p 2376 (2022)
Multi-hole probes can simultaneously measure the velocity and direction of a flow field, obtain the distribution of the flow field in a three-dimensional space, and obtain the vortex information in the flow field. Moreover, a multi-hole probe needs t
Externí odkaz:
https://doaj.org/article/7f4a10c313f74a6c88a5a45f6d4e1907
Publikováno v:
Sensors, Vol 21, Iss 18, p 6218 (2021)
Ice accretion or icing is a well-known phenomenon that entails a risk for the correct functioning of an aircraft. One of the areas more vulnerable to icing is the air data measuring system. This paper studies the icing protection offered by a heating
Externí odkaz:
https://doaj.org/article/546a815d813044aaac13899e8f959bd2
Publikováno v:
Sensors
Volume 21
Issue 18
Sensors, Vol 21, Iss 6218, p 6218 (2021)
Sensors (Basel, Switzerland)
Volume 21
Issue 18
Sensors, Vol 21, Iss 6218, p 6218 (2021)
Sensors (Basel, Switzerland)
Ice accretion or icing is a well-known phenomenon that entails a risk for the correct functioning of an aircraft. One of the areas more vulnerable to icing is the air data measuring system. This paper studies the icing protection offered by a heating
Autor:
Yang, Yihong
Stirring tanks are very important equipments used for mixing, separating, chemical reaction, etc. A typical stirring tank is a cylindrical vessel with an agitator driving the fluid and generating turbulence to promote mixing. Flotation cells are wide
Externí odkaz:
http://hdl.handle.net/10919/77056
http://scholar.lib.vt.edu/theses/available/etd-05022011-071449/
http://scholar.lib.vt.edu/theses/available/etd-05022011-071449/
Autor:
Jonsson, Isak
In commercial aviation, efficiency improvements may be gained by aerodynamic optimisation of its structural components, such as the intermediate compressor duct (ICD) and the turbine rear structure (TRS). These components have frequently been overloo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______4160::5fe2629160614d93cfb2038a25815122
https://research.chalmers.se/en/publication/527645
https://research.chalmers.se/en/publication/527645
Akademický článek
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Akademický článek
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Autor:
Pleiman, Brock Joseph
In airframe propulsion integration, the pressure recovered at the beginning of the inlet in comparison to the end of the inlet is a critical design point. Studies conducted by the Air Force Research Lab show that a loss in recovery pressure directly
Autor:
Bartsch, Christian
Publikováno v:
München : Hut, Messtechnik 1 Online-Ressource (xix, 161 Seiten) : Illustrationen, Diagramme (2017). doi:10.18154/RWTH-2017-09369 = Dissertation, RWTH Aachen University, 2017
Subject of the work presented here is a flow-adaptive measurement grid algorithm developed for one-dimensional (1D) and two-dimensional (2D) flow field surveys with pneumatic probes in turbomachinery flows. The algorithm automatically determines the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od_______791::2811ef10a8ee7b4776c31ce73a4a33dd
https://publications.rwth-aachen.de/record/707694
https://publications.rwth-aachen.de/record/707694
Akademický článek
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