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  • 1
    Online Resource
    Online Resource
    ASME International ; 1996
    In:  Journal of Fluids Engineering Vol. 118, No. 1 ( 1996-03-01), p. 123-127
    In: Journal of Fluids Engineering, ASME International, Vol. 118, No. 1 ( 1996-03-01), p. 123-127
    Abstract: Rotating stalls in vaneless diffusers are studied from the viewpoint that they are basically two-dimensional inviscid flow instability under the boundary conditions of vanishing velocity disturbance at the diffuser inlet and of vanishing pressure disturbance at the diffuser outlet. The linear analysis in the present report shows that the critical flow angle and the propagation velocity are functions of only the diffuser radius ratio. It is shown that the present analysis can reproduce most of the general characteristics observed in experiments: critical flow angle, propagation velocity, velocity, and pressure disturbance fields. It is shown that the vanishing velocity disturbance at the diffuser inlet is caused by the nature of impellers as a “resistance” and an “inertial resistance,” which is generally strong enough to suppress the velocity disturbance at the diffuser inlet. This explains the general experimental observations that vaneless diffuser rotating stalls are not largely affected by the impeller.
    Type of Medium: Online Resource
    ISSN: 0098-2202 , 1528-901X
    Language: English
    Publisher: ASME International
    Publication Date: 1996
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  • 2
    Online Resource
    Online Resource
    ASME International ; 2001
    In:  Journal of Fluids Engineering Vol. 123, No. 4 ( 2001-12-01), p. 762-770
    In: Journal of Fluids Engineering, ASME International, Vol. 123, No. 4 ( 2001-12-01), p. 762-770
    Abstract: A set of 4-bladed inducers with various amounts of cutback was tested with the aim of suppressing the rotating cavitation by applying alternate leading edge cutback. Unsteady cavitation patterns were observed by means of inlet pressure measurements and high-speed video pictures. It was found that the region with the alternate blade cavitation and asymmetric cavitation were enlarged with the increase of the amount of the cutback. As a result, the region with the rotating cavitation was diminished. At low flow rate, two types of alternate blade cavitation were found as predicted theoretically on 4-bladed inducer with smaller uneven blade length. One of them is with longer cavities on longer blades, and the other is with longer cavities on shorter blades. Switch was observed in these alternate blade cavitation patterns depending whether the cavitation number was increased or decreased. For an inducer with larger amount of cutback, the rotating cavitation and cavitation surge were almost suppressed as expected for a wide range of flow rate and cavitation number, although the cavitation performance was deteriorated. However, we should note that an asymmetric cavitation pattern occurs more easily in inducers with alternate leading edge cutback, and that the unevenness due to the cutback causes uneven blade stress.
    Type of Medium: Online Resource
    ISSN: 0098-2202 , 1528-901X
    Language: English
    Publisher: ASME International
    Publication Date: 2001
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  • 3
    Online Resource
    Online Resource
    Hindawi Limited ; 1997
    In:  International Journal of Rotating Machinery Vol. 3, No. 4 ( 1997), p. 259-268
    In: International Journal of Rotating Machinery, Hindawi Limited, Vol. 3, No. 4 ( 1997), p. 259-268
    Abstract: Detailed flow measurements have been made to clarify the unsteady flow in the backshroud/ casing clearance of a precessing centrifugal impeller. The unsteady pressure was integrated to obtain the fluid force moment on the precessing impeller shroud for various precessing frequencies. It was shown that the fluid force moment can become rotordynamically destabilizing for small forward precessing motion as originally found by Ohashi et al. The effects of leakage flow in the backshroud/casing clearance and a gap between impeller side plate and casing at the impeller outlet are clearly shown, and the discussions are also made based on the unsteady velocity and pressure measurements.
    Type of Medium: Online Resource
    ISSN: 1023-621X
    Language: English
    Publisher: Hindawi Limited
    Publication Date: 1997
    detail.hit.zdb_id: 2032559-9
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  • 4
    Online Resource
    Online Resource
    Japan Society of Mechanical Engineers ; 1994
    In:  TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B Vol. 60, No. 580 ( 1994), p. 4074-4081
    In: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, Japan Society of Mechanical Engineers, Vol. 60, No. 580 ( 1994), p. 4074-4081
    Type of Medium: Online Resource
    ISSN: 0387-5016 , 1884-8346
    Language: English
    Publisher: Japan Society of Mechanical Engineers
    Publication Date: 1994
    detail.hit.zdb_id: 2266820-2
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  • 5
    Online Resource
    Online Resource
    ASME International ; 2003
    In:  Journal of Fluids Engineering Vol. 125, No. 5 ( 2003-09-01), p. 786-795
    In: Journal of Fluids Engineering, ASME International, Vol. 125, No. 5 ( 2003-09-01), p. 786-795
    Abstract: This paper reports an experimental investigation of the rotordynamic fluid force and moment on a centrifugal impeller with three types of wear-ring seals; i.e., a face seal and two types of toothed seals. The impeller is equipped with a vaneless diffuser. Rotordynamic fluid forces and moments on the impeller in whirling motion were measured directly by using four-axis force sensor. Unsteady pressures were measured at several locations in the diffuser. It was found that, (1) at low flow rate, the fluid force and fluid force moment become maximum at a certain whirling speed caused by a coupling between the whirl motion and vaneless diffuser rotating stall and (2) the seal geometry with axial seal affects the direction of the coupled fluid force relative to the direction of eccentricity through the change in the unsteady leakage flow due to the whirl.
    Type of Medium: Online Resource
    ISSN: 0098-2202 , 1528-901X
    Language: English
    Publisher: ASME International
    Publication Date: 2003
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  • 6
    Online Resource
    Online Resource
    Hindawi Limited ; 2001
    In:  International Journal of Rotating Machinery Vol. 7, No. 4 ( 2001), p. 237-251
    In: International Journal of Rotating Machinery, Hindawi Limited, Vol. 7, No. 4 ( 2001), p. 237-251
    Abstract: In recent years, increasing interest has been given to the rotordynamic fluid forces on impellers, from the view point of the shaft vibration analysis. Previous experimental and analytical results have shown that the fluid-induced forces and moments on closed type pump impellers contribute substantially to the potential destabilization of subsynchronous shaft vibrations. However, to date few papers are known of the rotordynamic fluid forces on open-type centrifugal impellers. This paper reports about experimental investigations of the rotordynamic fluid force moments on an open-type centrifugal compressor impeller in precessing motion. For open-type impellers, the variations of the tip clearance and the clearance between the back shroud and casing due to the precessing motion contribute to the rotordynamic fluid force moments. Experiments were conducted to measure the rotordynamic fluid force moments directly using the 4-axis sensor, and the unsteady pressure on the front and back casing wall. In this paper, following results are obtained: (1) The fluid force moment becomes destabilizing in the region of negative precessing speed ratio ( - 0.3 〈 Ω / ω 〈 0 ) , at the design flow rate; (2) At reduced flow rate, the destabilizing fluid force moments occurred at small positive precessing speed ratio ( 0.2 〈 Ω / ω 〈 0.4 ) ; (3) From the comparison of direct measured fluid force moments with those estimated from the unsteady pressure measured on the front and back casing walls, it was found that the destabilizing moments in the backward precession are mainly caused by the fluid forces on the front surface of the present impeller, where there is large clearance between the back shroud and casing.
    Type of Medium: Online Resource
    ISSN: 1023-621X
    Language: English
    Publisher: Hindawi Limited
    Publication Date: 2001
    detail.hit.zdb_id: 2032559-9
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  • 7
    Online Resource
    Online Resource
    Hindawi Limited ; 2001
    In:  International Journal of Rotating Machinery Vol. 7, No. 6 ( 2001), p. 397-404
    In: International Journal of Rotating Machinery, Hindawi Limited, Vol. 7, No. 6 ( 2001), p. 397-404
    Abstract: It is well known that leading edge sweep has a favorable effect on the cavitation of turbomachines. However, the mechanisms of the improvement have not been made clear. It has been shown that the lift and the drag on a cavitating swept single hydrofoil can be correlated fairly well based on the velocity component normal to the leading edge. In the present paper, such correlations for swept cascades are derived and the results are examined, neglecting the full geometrical effects of the inducer rotor. It is shown that the correlations can simulate the developments of various types of cavitation, including alternate blade cavitation, rotating cavitation, and cavitation surge. This result is based on the observation that the steady cavity length, as well as the developments ofvarious types ofcavitation, is fairly well predicted by the correlation.
    Type of Medium: Online Resource
    ISSN: 1023-621X
    Language: English
    Publisher: Hindawi Limited
    Publication Date: 2001
    detail.hit.zdb_id: 2032559-9
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  • 8
    Online Resource
    Online Resource
    Hindawi Limited ; 2004
    In:  International Journal of Rotating Machinery Vol. 10, No. 4 ( 2004), p. 241-251
    In: International Journal of Rotating Machinery, Hindawi Limited, Vol. 10, No. 4 ( 2004), p. 241-251
    Abstract: In the present study, a higher order rotating cavitation predicted by the stability analysis was identified through the measurements of inlet pressure fluctuations and blade stress fluctuations. The propagation speed ratio of the higher order rotating cavitation is approximately 5, and the amplitude of the blade stress fluctuation caused by this rotating cavitation is the same level as that by the conventional rotating cavitation. In addition, a higher order cavitation surge was observed at the transition point from the conventional to the higher order rotating cavitation.
    Type of Medium: Online Resource
    ISSN: 1023-621X
    Language: English
    Publisher: Hindawi Limited
    Publication Date: 2004
    detail.hit.zdb_id: 2032559-9
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  • 9
    Online Resource
    Online Resource
    ASME International ; 1997
    In:  Journal of Fluids Engineering Vol. 119, No. 4 ( 1997-12-01), p. 775-781
    In: Journal of Fluids Engineering, ASME International, Vol. 119, No. 4 ( 1997-12-01), p. 775-781
    Abstract: Oscillating cavitation of an inducer was observed through unsteady inlet pressure measurements and by use of high speed video picture, covering a wide range of flow coefficient and cavitation number. One of the purposes of the study is to identify a mode of rotating cavitation predicted by a linear analysis, and the other is to obtain a general view of oscillating cavitation. The number of rotating cavitation cells and their propagation velocity were carefully determined from the phase difference of pressure fluctuations at various circumferential locations. Various kinds of oscillating cavitation were observed: rotating cavitation rotating faster/slower than impeller rotation, cavitation in backflow vortices, and surge mode oscillations. Effects of inlet and outlet (effective) pipelength were also studied.
    Type of Medium: Online Resource
    ISSN: 0098-2202 , 1528-901X
    Language: English
    Publisher: ASME International
    Publication Date: 1997
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  • 10
    Online Resource
    Online Resource
    ASME International ; 1997
    In:  Journal of Fluids Engineering Vol. 119, No. 2 ( 1997-06-01), p. 366-371
    In: Journal of Fluids Engineering, ASME International, Vol. 119, No. 2 ( 1997-06-01), p. 366-371
    Abstract: Experimental results of fluid moment on a centrifugal impeller shroud in precessing motion are discussed based on the bulk flow model to elucidate the fundamental flow mechanism. It is shown that the backshroud/casing clearance flow and the destabilizing fluid force moment can be simulated by the bulk flow model fairly well if the measured behavior of the resistance is correctly incorporated in the model. From the calculations with and without steady and unsteady wall shear stresses, the unsteady component of the clearance flow is shown to be basically a two-dimensional inviscid flow induced by the change in the flow thickness. The effects of the leakage flow rate and the resistance at the leakage flow entry are discussed, paying attention to the steady tangential velocity of the leakage flow.
    Type of Medium: Online Resource
    ISSN: 0098-2202 , 1528-901X
    Language: English
    Publisher: ASME International
    Publication Date: 1997
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