Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Florian Hoefler"'
Autor:
Martin Bitter, Reinhard Niehuis, Svenja Aberle, Florian Hoefler, Jorge Alejandro Carretero Benignos
Publikováno v:
17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC2017)
17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC2017), Dec 2017, Maui, United States
17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC2017), Dec 2017, Maui, United States
For heat transfer measurements on the center blade of a linear cascade, the infrared measurement technique was set up. As a highly challenging condition, the angular dependency of the infrared signal was identified. Beside a shallow angle of view, li
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::febfab3e6f6e0a232b2aeb1f190cfac4
https://hal.science/hal-02397983
https://hal.science/hal-02397983
Autor:
Florian Hoefler, David Helmer
Publikováno v:
Volume 5A: Heat Transfer.
A steady-state IR measurement is described and demonstrated for a leading edge crossover impingement configuration. Thin-walled leading edge models are used, with a constant heat flux boundary condition generated. This approach allows for rapid and l
Publikováno v:
Journal of Turbomachinery. 134
Heat transfer measurements of a confined impingement cooling configuration with ribs on the target surfaces are presented. The assembly consists of four non-perpendicular walls of which one holds two rows of staggered inclined jets, each impinging on
Publikováno v:
Volume 5: Heat Transfer, Parts A and B.
Experimental and numerical heat transfer results in a trapezoidal duct with two staggered rows of inclined impingement jets are presented. The influence of changes in the jet bore geometry on the wall heat transfer is examined. The goal of this proje
Publikováno v:
2010 14th International Heat Transfer Conference, Volume 5.
A confined jet impingement configuration has been investigated in which the matter of interest is the convective heat transfer from the air flow to the passage walls. The geometry is similar to gas turbine blade cooling applications. The setup is dis
Publikováno v:
Volume 3: Heat Transfer, Parts A and B.
Impingement cooling is widely used in cooling configurations for gas turbine components. Relatively high local heat transfer rates and the possibility of jet adjustment to specific geometries are advantageous for internal turbine blade cooling design