Geometrical uncertainty in turbomachinery: Tip gap and fillet radius-Reference-Cited by-同舟云学术

Geometrical uncertainty in turbomachinery: Tip gap and fillet radius

Published:2011-07 Issue:1 Volume:46 Page:362-368
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Montomoli F.,Massini M.,Salvadori S.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference20 articles.

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3. Heat transfer and flow on the first-stage blade tip of a power generation gas turbine. Part 2: Simulation results;Ameri;ASME J Turbomach,2000

4. Adami P, Martelli F, Michelassi V. Three-dimensional investigations for axial turbines by an implicit unstructured multi-block flow solver. In: Proceedings of the ASME-IGTI turbo expo 2000, Munich, DE; 2000.

5. Adami P, Michelassi V, Martelli F. Performances of a NewtonKrylov scheme against implicit and multi-grid solvers for inviscid flows. In: AIAA paper; 1998. p. 98–2429.

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