Fatigue of Aircraft Structures > 2021 > Iss. 13 > 40--53
Source
Abstract
Identifiers
journal ISSN : | 2081-7738 |
journal e-ISSN : | 2300-7591 |
DOI | 10.2478/fas-2021-0005 |
Authors
Keywords
Additional information
Fields of science
Bibliography
-
[1] Beretta-Müller, A. & Szwedowicz, J. (2015). Blade Resonant Forced Response Excited by Combustor Acoustic Eigenmodes. In: Proceedings of ASME Turbo Expo: Turbine Technical Conference and Exposition, June 15 - 19, 2015, Montreal, Quebec, Canada.
-
[2] Corral, R. (2012). Bladed Disks: Flutter, Structural Design of Aircraft Engines, RTO-AVT-207-06, 25 January, Belgium.
-
[3] Dodds, J., and Vahdati, M. (May 1, 2015). Rotating Stall Observations in a High Speed Compressor-Part II: Numerical Study. ASME. J. Turbomach. May 2015, Vol. 137, No. 5, 051003. DOI: 10.1115/1.4028558.