1. Raeesi Estabregh E, Ziaee Rad S. The worst response of mistuned bladed disk system using genetic algorithm. Amirkabir Journal of Mechanical Engineering. 2013;44(2):41-51. [Persian] [
Link]
2. Wei ST, Pierre C. Localization phenomena in mistuned assemblies with cyclic symmetry part I: Free vibrations. Journal of Vibration Acoustics Stress and Reliability in Design. 1988;110(4):429-438. [
Link] [
DOI:10.1115/1.3269547]
3. Srinivasan AV. Influence of mistuning on blade torsional flutter [Internet]. Washington DC: NASA Technical Reports Server; 1980 [cited 2018 April 14]. Available from: https://ntrs.nasa.gov/search.jsp?R=19800022846 [
Link]
4. Smith SN. Discrete frequency sound generation in axial flow turbomachines [Dissertation]. London: University of Cambridge; 1971. [
Link]
5. Kaza KRV, Kielb RE. Flutter and response of a mistuned cascade in incompressible flow. AIAA Journal. 1982;20(8):1120-1127. [
Link] [
DOI:10.2514/3.51172]
6. Kaza KRV, Kielb RE. Flutter of turbofan rotors with mistuned blades. AIAA Journal. 1984;22(11):1618-1625. [
Link] [
DOI:10.2514/3.8827]
7. Kaza KRV, Kielb RE. Vibration and flutter of mistuned bladed-disk assemblies. Journal of Propulsion and Power. 1985;1(5):336-344. [
Link] [
DOI:10.2514/3.22806]
8. Whiteman WE, Ferri AA. Suppression of bending-torsion flutter through displacement-dependent dry friction damping. AIAA Journal. 1999;37(1):79-83.
https://doi.org/10.2514/3.14126 [
Link] [
DOI:10.2514/2.667]
9. Crouse GL, Leishman JG. Transonic aeroelasticity analysis using state-space unsteady aerodynamic modeling. Journal of Aircraft. 1992;29(1):153-160. [
Link] [
DOI:10.2514/3.46139]
10. Gordon Leishman J, Crouse Jr GL. A state-space model of unsteady aerodynamics in a compressible flow for flutter analyses. 27th Aerospace Sciences Meeting, 9-12 January 1989, Reno, NV, USA. Reston VA: AIAA; 1989. [
Link] [
DOI:10.2514/6.1989-22]
11. Pierre C, Murthy DV. Aeroelastic modal characteristics of mistuned blade assemblies-mode localization and loss of eigenstructure. AIAA Journal. 1992;30(10):2483-2496. [
Link] [
DOI:10.2514/3.11251]
12. Pierre C, Smith TE, Murthy DV. Localization of aeroelastic modes in mistuned high-energy turbines. Journal of Propulsion and Power. 1994;10(3):318-328. [
Link] [
DOI:10.2514/3.23759]
13. Whitehead D. Force and moment coefficients for vibrating airfoils in cascade [Internet]. London: Her Majesty's Stationery Office; 1962 [cited 2018 April 14]. Available from: http://citeseerx.ist.psu.edu/viewdoc/download?doi=10.1.1.226.7404&rep=rep1&type=pdf [
Link]
14. Whitehead DS. Effect of mistuning on the vibration of turbo-machine blades induced by wakes. Journal of Mechanical Engineering Science. 1966;8(1):15-21. [
Link] [
DOI:10.1243/JMES_JOUR_1966_008_004_02]
15. Bendiksen O, Friedmann P. Coupled bending-torsion flutter in cascades. AIAA Journal. 1980;18(2):194-201. [
Link] [
DOI:10.2514/3.50748]
16. Adamczyk JJ, Goldstein ME. Unsteady flow in a supersonic cascade with subsonic leading-edge locus. AIAA Journal. 1978;16(12);1248-1254. [
Link] [
DOI:10.2514/3.61040]
17. Ananth SM, Kushari A, Venkatesan C. Quasi-steady prediction of coupled bending-torsion flutter under rotating stall. Journal of Fluids and Structures. 2013;43:402-427. [
Link] [
DOI:10.1016/j.jfluidstructs.2013.09.004]
18. Castanier MP, Pierre C. Modeling and analysis of mistuned bladed disk vibration: Current status and emerging directions. Journal of Propulsion and Power. 2006;22(2):384-396. [
Link] [
DOI:10.2514/1.16345]
19. Yang MT, Griffin JH. A reduced-order model of mistuning using a subset of nominal system modes. Journal of Engineering for Gas Turbines and Power. 2001;123(4):893-900. [
Link] [
DOI:10.1115/1.1385197]
20. Olson BJ, Shaw SW, Shi C, Pierre C, Parker RG. Circulant matrices and their application to vibration analysis. Applied Mechanics Reviews. 2014;66(4):040803. [
Link] [
DOI:10.1115/1.4027722]