2005
DOI: 10.1007/s10697-005-0041-4
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Calculation of the unsteady aerodynamic parameters of a rotating cascade of oscillating blades in incompressible flow

Abstract: The unsteady aerodynamic parameters of 3D blade cascades oscillating in incompressible flow are determined with account for blade geometry and the influence of the steady hydrodynamic loads acting on the blades. On the assumption of separationless flow and harmonic blade oscillations, the corresponding boundary-value problem for the amplitude function of the unsteady velocity potential component is solved in the linear formulation, using a finite-element method. Test calculation results are presented and an ex… Show more

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Cited by 3 publications
(4 citation statements)
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“…Figure 2 shows the amplitudes of vibrations averaged over the period T = 100 sec, which were obtained not long before the accident (A x , A y , and A z are the amplitudes of vibrations in the directions from north to south, from east to west, and along the turbine axis, respectively). Forced vibrations with frequencies (9) can be seen at Ω 0 = 2.38 Hz and Ω v = 0.5-1.5 Hz. The level of these vibrations is rather high, obviously, because their frequencies are close to the frequencies of natural hydroacoustic oscillations (8).…”
Section: Comparison Of Theoretical and Experimental Resultsmentioning
confidence: 98%
See 1 more Smart Citation
“…Figure 2 shows the amplitudes of vibrations averaged over the period T = 100 sec, which were obtained not long before the accident (A x , A y , and A z are the amplitudes of vibrations in the directions from north to south, from east to west, and along the turbine axis, respectively). Forced vibrations with frequencies (9) can be seen at Ω 0 = 2.38 Hz and Ω v = 0.5-1.5 Hz. The level of these vibrations is rather high, obviously, because their frequencies are close to the frequencies of natural hydroacoustic oscillations (8).…”
Section: Comparison Of Theoretical and Experimental Resultsmentioning
confidence: 98%
“…In non-separated flow around the blades, the classical flutter of turbomachine cascades is known to arise at Strouhal numbers much lower than in separated flow regimes. An approximate solution of the corresponding problem of an unsteady flow of a cascade with an arbitrary geometry can be constructed within the framework of the incompressible fluid model, for instance, by the method developed in [9]. The classical flutter is almost impossible in the case of vibrations of a cascade with one degree of freedom; therefore, the probability of emergence of instability of hydroacoustic oscillations in these regimes is rather low.…”
mentioning
confidence: 99%
“…In fact, there exit some literatures to study the problems in the transient stability of the non‐linear MUHGSs. Such problems involve the structure optimisation [23], fault diagnosis [24], system parameter setting [25] and the analysis of start‐up opening laws [] etc. However, the fact is that the researcher faces great challenges due to the complex non‐linearity of the MUHGS, such as, the non‐linear effect of surge tanks, the water hammer in penstocks and the shafting vibration.…”
Section: Introductionmentioning
confidence: 99%
“…Starting from a series of papers [26][27][28][29] as well as [30,31], several 3-D aeroelastic codes have been developed by different researchers during the last decade [32][33][34][35][36][37]. Most of them are based on the energy method, though there are some employing time-domain and eigenfrequency calculations.…”
Section: Introductionmentioning
confidence: 99%