Steady and unsteady numerical investigation of transitional shock-boundary-layer-interactions on a fan blade-Reference-Cited by-同舟云学术

Steady and unsteady numerical investigation of transitional shock-boundary-layer-interactions on a fan blade

Published:2007-11 Issue:7-8 Volume:11 Page:507-517
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Becker B.,Reyer M.,Swoboda M.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference12 articles.

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3. The design of an advanced civil fan rotor;Ginder;ASME Trans. J. Turbomach.,1987

4. Th. Hildebrandt, M. Swoboda, E. Lorrain, Steady and unsteady transitional 3D Navier–Stokes calculation of a 1,5-stage axial low speed compressor, in: Proceedings of 17th International Symposium on Airbreathing Engines, 4–9 September 2005, Munich, Germany, 2005

5. A. Jameson, T.J. Baker, Multigrid solution of the Euler equations for aircraft configurations, AIAA Paper 84-00931984, 1984

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