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Soltani Dehkharqani, ArashORCID iD iconorcid.org/0000-0001-5143-7729
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Publications (7 of 7) Show all publications
Soltani Dehkharqani, A., Aidanpää, J.-O., Engström, F. & Cervantes, M. (2019). Fluid added polar inertia and damping for the torsional vibration of a Kaplan turbine model runner considering multiple perturbations. In: IOP Conference Series: Earth and Environmental Science. Paper presented at 29th IAHR Symposium on Hydraulic Machinery and Systems, 17-21 September 2018, Kyoto, Japan.. Institute of Physics (IOP), 240, Article ID 062007.
Open this publication in new window or tab >>Fluid added polar inertia and damping for the torsional vibration of a Kaplan turbine model runner considering multiple perturbations
2019 (English)In: IOP Conference Series: Earth and Environmental Science, Institute of Physics (IOP), 2019, Vol. 240, article id 062007Conference paper, Published paper (Refereed)
Abstract [en]

A water turbine runner is exposed to several perturbation sources with differentfrequencies, phases, and amplitudes both at the design and off-design operations. Rotor-statorinteraction, cavitation, rotating vortex rope, and blade trailing edge vortices are examples of suchperturbations which can disturb the runner. The rotor dynamic coefficients require beingdetermined to perform a reliable dynamic analysis. Fluid added inertia, damping, and stiffnesshave previously been investigated for individual perturbation frequencies for the torsionalvibration of a Kaplan turbine model runner. However, a number of perturbation sources mostlytake place simultaneously and alter the dynamics of the runner. Soltani et al. [1] have evaluatedthe torsional added parameters for a Kaplan turbine runner using numerical simulationsconsidering single perturbation frequency. In the present work, the fluid added parameters areassessed in the presence of multiple perturbation sources. A similar methodology is used. Asingle-degree-of-freedom (SDOF) model for the dynamic model and unsteady ReynoldsaveragedNavier–Stokes approach for the flow simulations are assumed. Perturbations withdifferent frequencies are applied to the rotational speed of the runner to determine the fluid addedparameters for the torsional vibration. A number of previously investigated frequencies arechosen and their combinations are investigated. In addition, two different phase shifts areconsidered between the applied perturbations to study the effect of phase. Two more test caseswith higher perturbation amplitude are also conducted to investigate its influence on the fluidadded inertia and damping. The results are compared with the previous study and the interactionof multiple perturbations on the added parameters is investigated.

Place, publisher, year, edition, pages
Institute of Physics (IOP), 2019
National Category
Mechanical Engineering Fluid Mechanics and Acoustics Other Mechanical Engineering
Research subject
Fluid Mechanics; Computer Aided Design
Identifiers
urn:nbn:se:ltu:diva-72503 (URN)10.1088/1755-1315/240/6/062007 (DOI)2-s2.0-85063961671 (Scopus ID)
Conference
29th IAHR Symposium on Hydraulic Machinery and Systems, 17-21 September 2018, Kyoto, Japan.
Available from: 2019-01-09 Created: 2019-01-09 Last updated: 2019-06-26Bibliographically approved
Soltani Dehkharqani, A., Aidanpää, J.-O., Engström, F. & Cervantes, M. (2018). A Review of Available Methods for the Assessment of Fluid Added Mass, Damping, and Stiffness With an Emphasis on Hydraulic Turbines. Applied Mechanics Review, 70(5), Article ID 050801.
Open this publication in new window or tab >>A Review of Available Methods for the Assessment of Fluid Added Mass, Damping, and Stiffness With an Emphasis on Hydraulic Turbines
2018 (English)In: Applied Mechanics Review, ISSN 0003-6900, E-ISSN 1088-8535, Vol. 70, no 5, article id 050801Article in journal (Refereed) Published
Abstract [en]

Fluid added mass, damping, and stiffness are highly relevant parameters to consider when evaluating the dynamic response of a submerged structure in a fluid. The prediction of these parameters for hydraulic turbines has been approached relatively recently. Complex fluid-structure analyses including three-dimensional flow and the need for experiments during operation are the main challenges for the numerical and experimental approaches, respectively. The main objective of this review is to address the impact of different parameters, for example, flow velocity, cavitation, nearby solid structure, and rotational speed on the fluid added mass and damping of Kaplan/Propeller and Francis turbine runners. The fluid added stiffness is also discussed in the last section of the paper. Although studies related to hydraulic turbines are the main objective of this paper, the literature on hydrofoils is also taken into consideration to provide valuable information on topics such as individual runner blades. In this literature survey, the analytical, numerical, and experimental approaches used to determine fluid added parameters are discussed, and the pros and the cons of each method are addressed.

Place, publisher, year, edition, pages
ASME Press, 2018
Keywords
fluid added mass, fluid added damping, fluid added stiffness, Francis turbine, Kaplan turbine, hydrofoils
National Category
Fluid Mechanics and Acoustics Other Mechanical Engineering
Research subject
Fluid Mechanics; Computer Aided Design
Identifiers
urn:nbn:se:ltu:diva-72502 (URN)10.1115/1.4042279 (DOI)000458511300001 ()2-s2.0-85059957623 (Scopus ID)
Note

Validerad;2019;Nivå 2;2019-01-29 (svasva)

Available from: 2019-01-09 Created: 2019-01-09 Last updated: 2019-08-26Bibliographically approved
Soltani Dehkharqani, A., Cervantes, M. & Aidanpää, J.-O. (2017). Numerical analysis of fluid-added parameters for the torsional vibration of a Kaplan turbine model runner. Advances in Mechanical Engineering, 9(10), Article ID 1687814017732893.
Open this publication in new window or tab >>Numerical analysis of fluid-added parameters for the torsional vibration of a Kaplan turbine model runner
2017 (English)In: Advances in Mechanical Engineering, ISSN 1687-8132, E-ISSN 1687-8140, Vol. 9, no 10, article id 1687814017732893Article in journal (Refereed) Published
Abstract [en]

The impact of fluid on the runner of a hydraulic turbine is a recurrent problem. Fully coupled fluid-structure simulations are extremely time consuming. Thus, an alternative method is required to estimate this interaction to perform a reliable rotor dynamic analysis. In this paper, numerical estimations of the added inertia, damping and stiffness for a Kaplan turbine model runner are presented using transient-flow simulations. A single-degree-of-freedom model was assumed for the fluid-runner interaction, and the parameters were estimated by applying a harmonic disturbance to the angular velocity of the runner. The results demonstrate that the added inertia and damping are important, whereas the stiffness is negligible. The dimensionless added polar inertia is 23-27% of the reference value (ρR5). Damping significantly contributes to the moment at low excitation frequencies, whereas the inertia becomes dominant at higher frequencies.

Place, publisher, year, edition, pages
Sage Publications, 2017
National Category
Fluid Mechanics and Acoustics Other Mechanical Engineering
Research subject
Fluid Mechanics; Computer Aided Design
Identifiers
urn:nbn:se:ltu:diva-66314 (URN)10.1177/1687814017732893 (DOI)000413891200001 ()2-s2.0-85033435074 (Scopus ID)
Note

Validerad;2017;Nivå 2;2017-11-09 (andbra)

Available from: 2017-10-30 Created: 2017-10-30 Last updated: 2018-12-14Bibliographically approved
Dehkharqani, A. S., Amiri, K. & Cervantes, M. (2015). Steady and transient pressure measurements on the runner blades of a Kaplan turbine model (ed.). Paper presented at IAHR meeting of the Working Group “Cavitation and dynamic problems" : 09/09/2015 - 11/09/2015. Paper presented at IAHR meeting of the Working Group “Cavitation and dynamic problems" : 09/09/2015 - 11/09/2015.
Open this publication in new window or tab >>Steady and transient pressure measurements on the runner blades of a Kaplan turbine model
2015 (English)Conference paper, Oral presentation only (Refereed)
Abstract [en]

The development of renewable energy sources has increased the need for power regulation. Power system regulation is mainly performed by hydropower plants through load variations. Additional forces are exerted on the runner blades during these load variations. This paper deals with pressure measurement performed on the blades of a Kaplan turbine model under steady state and load variation conditions. Flow behavior and frequency content of the pressure are investigated and compared to find critical condition in terms of pressure fluctuation. The results show that at various operating points and conditions, different regions of the blade are important. During load rejection, a considerable amount of pressure fluctuations are exerted on the runner blades. These results will be used to define experiments to be performed on the corresponding prototype. On the prototype, the loads acting on the runner blades will be investigated at various operation points similar to the model. In addition, the relation between the frequency content on the blades and loads on the main shaft will be investigated. Comparing results from model and prototype eventually would be valuable to explore the flow characteristics in prototype since CFD simulation of prototype is challenging.

National Category
Fluid Mechanics and Acoustics
Research subject
Fluid Mechanics
Identifiers
urn:nbn:se:ltu:diva-26989 (URN)0483c990-33a4-4860-b187-6204b09379e3 (Local ID)0483c990-33a4-4860-b187-6204b09379e3 (Archive number)0483c990-33a4-4860-b187-6204b09379e3 (OAI)
Conference
IAHR meeting of the Working Group “Cavitation and dynamic problems" : 09/09/2015 - 11/09/2015
Note
Godkänd; 2015; 20150918 (arasol)Available from: 2016-09-30 Created: 2016-09-30 Last updated: 2017-11-29Bibliographically approved
Dehkharqani, A. S., Boroomand, M. & Eshraghi, H. (2014). A Numerical Investigation of Loss Coefficient Variation in Various Incidence Angles in Tandem Blades Cascade (ed.). In: (Ed.), (Ed.), A Numerical Investigation of Loss Coefficient Variation in Various Incidence Angles in Tandem Blades Cascade: . Paper presented at ASME 2014 International Mechanical Engineering Congress & Exposition : 14/11/2014 - 20/11/2014.
Open this publication in new window or tab >>A Numerical Investigation of Loss Coefficient Variation in Various Incidence Angles in Tandem Blades Cascade
2014 (English)In: A Numerical Investigation of Loss Coefficient Variation in Various Incidence Angles in Tandem Blades Cascade, 2014Conference paper, Published paper (Refereed)
Abstract [en]

There is a severe tendency to reduce weight and increase power of gas turbine. Such a requirement is fulfilled by higher pressure ratio of compressor stages. Employing tandem blades in multi-stage axial flow compressors is a promising methodology to control separation on suction sides of blades and simultaneously implement higher turning angle to achieve higher pressure ratio. The present study takes into account the high flow deflection capabilities of the tandem blades consisting of NACA-65 airfoil with fixed percent pitch and axial overlap at various flow incidence angles. In this regard, a two-dimensional cascade model of tandem blades is constructed in a numerical environment. The inlet flow angle is varied in a wide range and overall loss coefficient and deviation angles are computed. Moreover, the flow phenomena between the blades and performance of both forward and afterward blades are investigated. At the end, the aerodynamic flow coefficient of tandem blades are also computed with equivalent single blades to evaluate the performance of such blades in both design and off-design domain of operations. The results show that tandem blades are quite capable of providing higher deflection with lower loss in a wide range of operation and the base profile can be successfully used in design of axial flow compressor. In comparison to equivalent single blades, tandem blades have less dissipation because the momentum exerted on suction side of tandem blades confines the size of separation zone near trailing edges of blades.

National Category
Fluid Mechanics and Acoustics
Identifiers
urn:nbn:se:ltu:diva-32430 (URN)10.1115/IMECE2014-39881 (DOI)6ec6ea71-e553-4ff5-b292-0a503e4f1e1b (Local ID)6ec6ea71-e553-4ff5-b292-0a503e4f1e1b (Archive number)6ec6ea71-e553-4ff5-b292-0a503e4f1e1b (OAI)
Conference
ASME 2014 International Mechanical Engineering Congress & Exposition : 14/11/2014 - 20/11/2014
Note
Upprättat; 2014; 20150331 (arasol)Available from: 2016-09-30 Created: 2016-09-30 Last updated: 2017-11-29Bibliographically approved
Dehkharqani, A. S., Boroomand, M. & Eshraghi, H. (2013). A Numerical Investigation of Performance Parameter in 2-D Tandem Blade Cascade (ed.). In: (Ed.), (Ed.), A Numerical Investigation of Performance Parameter in 2-D Tandem Blade Cascade: . Paper presented at Annual International Conference on Mechanical Engineering, ISME-2013 : 07/05/2013 - 09/05/2013.
Open this publication in new window or tab >>A Numerical Investigation of Performance Parameter in 2-D Tandem Blade Cascade
2013 (Persian)In: A Numerical Investigation of Performance Parameter in 2-D Tandem Blade Cascade, 2013Conference paper, Published paper (Refereed)
National Category
Fluid Mechanics and Acoustics
Identifiers
urn:nbn:se:ltu:diva-38637 (URN)d144d030-1dbe-4302-b9f4-52eb5f06f2df (Local ID)d144d030-1dbe-4302-b9f4-52eb5f06f2df (Archive number)d144d030-1dbe-4302-b9f4-52eb5f06f2df (OAI)
Conference
Annual International Conference on Mechanical Engineering, ISME-2013 : 07/05/2013 - 09/05/2013
Note
Upprättat; 2013; 20150401 (arasol)Available from: 2016-10-03 Created: 2016-10-03 Last updated: 2017-11-29Bibliographically approved
Boroomand, M., Dehkharqani, A. S., Khelghatibana, M. & Vahidi, M. (2011). Preliminary design of axial flow compressors (ed.). In: (Ed.), (Ed.), Preliminary design of axial flow compressors: . Paper presented at Conference of Iranian Aerospace Society : 01/03/2011 - 03/03/2011.
Open this publication in new window or tab >>Preliminary design of axial flow compressors
2011 (Persian)In: Preliminary design of axial flow compressors, 2011Conference paper, Published paper (Refereed)
Identifiers
urn:nbn:se:ltu:diva-33138 (URN)7ed4508e-b6e9-41b7-98bb-8ad844458ff0 (Local ID)7ed4508e-b6e9-41b7-98bb-8ad844458ff0 (Archive number)7ed4508e-b6e9-41b7-98bb-8ad844458ff0 (OAI)
Conference
Conference of Iranian Aerospace Society : 01/03/2011 - 03/03/2011
Note
Upprättat; 2011; 20150401 (arasol)Available from: 2016-09-30 Created: 2016-09-30 Last updated: 2017-11-29Bibliographically approved
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Identifiers
ORCID iD: ORCID iD iconorcid.org/0000-0001-5143-7729

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