Uncertainty Quantification Applied to Gas Turbine Components-Reference-Cited by-同舟云学术

Uncertainty Quantification Applied to Gas Turbine Components

Published:2018-06-22 Issue: Volume: Page:157-193
ISSN:
Container-title:Uncertainty Quantification in Computational Fluid Dynamics and Aircraft Engines
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Author:

Montomoli Francesco,Massini M.

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-319-92943-9_4

Reference42 articles.

1. Goodhand, M. N., Miller, R. J., & Lung, H. W. (2012). The sensitivity of 2D compressor incidence range to in-service geometric variation. Proceedings of the ASME Turbo Expo, 8, 159–170.

2. Lange, A., Voigt, M., & Vogeler, K. (2012). Principal component analysis on 3D scanned compressor blades for probabilistic CFD simulation. 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012.

3. Seshadri, P., Parks, G., & Jarrett, J. (2013). Towards robust design of axial compressors with uncertainty quantification. Collection of Technical Papers—AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.

4. Seshadri, P., Shahpar, S., & Parks, G. T. (2014). Robust compressor blades for desensitizing operational tip clearance variations. Proceedings of ASME Turbo Expo 2014: Turbine Technical Conference and Exposition GT2014, June 16–20.

5. Giebmanns, A., Backhaus, J., & Frey, C. (2013) Compressor leading edge sensitivities and analysis with an adjoint flow solver. Proceedings of the ASME Turbo Expo, 6 A.

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