Search results

Filters

  • Journals
  • Authors
  • Keywords
  • Date
  • Type

Search results

Number of results: 10
items per page: 25 50 75
Sort by:
Download PDF Download RIS Download Bibtex

Abstract

The two dimensional steady and unsteady flow field at midspan in a low speed axial flow compressor stage has been investigated experimentally, using two systems, based on totally different principles: a 2-sensor fast response straight and 90° triple split fiber probes (TSFP) and two dimensional LOA system with an emphasis on the interaction of the inlet guide vane (IGY) wake with the rotor flow field. To account for the uniformity of the rotor absolute inlet flow field, measurements has been made at eight tangential locations in the absolute frame equally spaced over one IGY pitch. The time resolved investigation, done by TSFP and LOA allows to presenting velocity fields, flow angles and turbulence data at different [GY-rotor positions during one blade passing period. The velocity measurements are decomposed into a time averaged velocity, a periodic velocity component and a unresolved velocity component. Using two measurement systems, one being intrusive and the other non-intrusive, in the same complex flow field, gives the opportunity for a critical comparison of results and opens the view for further improvements. Averaging these results, enabled also comparison with the pneumatic five-hole probe measurement.
Go to article

Authors and Affiliations

Andrzej Witkowski
Mirosław Majkut
Download PDF Download RIS Download Bibtex

Abstract

The aim of this paper is to analyze various CO2 compression processes for post-combustion CO2 capture applications for 900 MW pulverized coal-fired power plant. Different thermodynamically feasible CO2 compression systems will be identified and their energy consumption quantified. A detailed thermodynamic analysis examines methods used to minimize the power penalty to the producer through integrated, low-power compression concepts. The goal of the present research is to reduce this penalty through an analysis of different compression concepts, and a possibility of capturing the heat of compression and converting it to useful energy for use elsewhere in the plant.

Go to article

Authors and Affiliations

Andrzej Witkowski
Mirosław Majkut
Download PDF Download RIS Download Bibtex

Abstract

Recently, significant progress has been made in experimental studies on the flow of wet steam, measuring techniques based on recording the phenomenon of extinction of light and ultrasound have been elaborated or improved. The basic value experimentally determined in the final stage was the content of the liquid phase defined as the wetness fraction. The methodology of tests and experimental investigations was presented, as well as the applied and developed measurement systems. Next, some developed designs of new ultrasonic and light extinction measuring probe and their modifications are described. The article presents also some examples of applications of the developed measurement techniques in application to experimental research conducted on wet steam. Examples of comparison between experimental and numerical tests for the extinction method are also provided.

Go to article

Authors and Affiliations

Mirosław Majkut
Sławomir Dykas
Krystian Smołka
Download PDF Download RIS Download Bibtex

Abstract

A commercially available ASPEN PLUS simulation using a pipe model was employed to determine the maximum safe pipeline distances to subsequent booster stations as a function of carbon dioxide (CO2) inlet pressure, ambient temperature and ground level heat flux parameters under three conditions: isothermal, adiabatic and with account of heat transfer. In the paper, the CO2working area was assumed to be either in the liquid or in the supercritical state and results for these two states were compared. The following power station data were used: a 900 MW pulverized coal-fired power plant with 90% of CO2recovered (156.43 kg/s) and the monothanolamine absorption method for separating CO2from flue gases. The results show that a subcooled liquid transport maximizes energy efficiency and minimizes the cost of CO2transport over long distances under isothermal, adiabatic and heat transfer conditions. After CO2is compressed and boosted to above 9 MPa, its temperature is usually higher than ambient temperature. The thermal insulation layer slows down the CO2temperature decrease process, increasing the pressure drop in the pipeline. Therefore in Poland, considering the atmospheric conditions, the thermal insulation layer should not be laid on the external surface of the pipeline.

Go to article

Authors and Affiliations

Andrzej Witkowski
Mirosław Majkut
Sebastian Rulik
Download PDF Download RIS Download Bibtex

Abstract

The paper presents a research program carried out to improve understanding of the fluid dynamics mechanisms that lead to rotating stall in the axial flow low speed compressor stage. The stalling behavior of this compressor stage was studied by measuring unsteady casing pressure by means of a circumferentially and axially spaced array of high frequency pressure transducers. Another probe used was a disc static pressure probe, with the pressure transducer, for in-flow and out-flow measurements along the blade span. It was expected that understanding of the fluid dynamics will facilitate at least two important tasks. The first was to accurately predict of when and how a particular compressor would stall. The second was to control, delay, or eventually suppress the rotating stall and surge. In consequence, one could extend the useful operating range of the axial compressor. Another motivation for the research was to compare the results from the three applied analysis techniques by using a single stall inception event. The first one was a simple visual inspection of the traces, which brought about a very satisfactory effect. The second one was application of spatial Fourier decomposition to the analysis of stall inception data, and the third method of analysis consisted in application of wavelet filtering in order to better understand the physical mechanisms which lead to rotating stall. It was shown that each of these techniques would provide different information about compressor stall behavior, and each method had unique advantages and limitations.

Go to article

Authors and Affiliations

Marcin Ziach
Mirosław Majkut
Andrzej Witkowski
Keywords Fan CFD Cyclorotor
Download PDF Download RIS Download Bibtex

Bibliography

[1] Morandini M., Xisto C., Pascoa J., Quaranta G., Gagnon L., Masarati P.: Aeroelastic analysis of a cycloidal rotor under various operating conditions. J. Aircraft. 55(2018), 4, 1675–1688.
[2] Muscarello V., Masarati P., Quaranta G., Georges T., Gomand J., Malburet F., Marilena P.: Instability mechanism of roll/lateral biodynamic rotorcraft–pilot couplings. J. Am. Helicopter Soc. 63(2018), 1–13.
[3] Xisto C. Leger J., Pascoa J., Gagnon L., Masarati P., Angeli D., Dumas A.: Parametric analysis of a large-scale cycloidal rotor in hovering conditions. J. Aerospace Eng. 30(2017), 1.
[4] Xisto C., Pascoa J., Abdollahzadeh M., Leger J., Masarati P., Gagnon L., Schwaiger M., Wills D.: PECyT – plasma enhanced cycloidal thruster. In: Proc. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. July 28–30, 2014, Cleveland.
[5] Andrisani A., Angeli D., Dumas A.: Optimal pitching schedules for a cycloidal rotor in hovering. Aircr. Eng. Aerosp. Tec. 88(2016), 5.
[6] Xisto C., Pascoa J., Leger J.: Cycloidal rotor propulsion system with plasma enhanced aerodynamics. In: Proc. ASME 2014 Int.l Mechanical Engineering Congress and Exposition; Montreal, Nov. 14–20, 2014; V001T01A005.
[7] Xisto C., Pascoa J., Trancossi M.: Geometrical parameters influencing the aerodynamic efficiency of a small-scale self-pitch high solidity VAWT. J. Sol. Energy Eng. 138(2016), 031006.
[8] Benedict M.: Fundamental understanding of cycloidal-rotor concept for micro air vehicle applications. PhD thesis, Univ. Maryland, College Park, 2010.
[9] Benedict M., Ramasamy M., Chopra I.: Improving the aerodynamic performance of micro-air-vehicle-scale cycloidal rotor: An experimental approach. J. Aircraft 47(20104), 1117–1125.
[10] Heimerl J., Halder A., Benedict M.: Experimental and computational investigation of a UAV-scale cycloidal rotor in forward flight. In: Proc. The Vertical Flight Society’s 77th Ann. Vertical Flight Society Forum and Technology Display, The Future of Vertical Flight, Virtual, May 10–14, 2021.
[11] Halder A., Benedict M.: Nonlinear aeroelastic coupled trim analysis of a twin cyclocopter in forward flight. AIAA J., 59, 2021, 305–319.
[12] Lee B., Saj V., Benedict M., Kalathil D.: A Vision-Based Control Method for Autonomous Landing Of Vertical Flight Aircraft On A Moving Platform Without Using GPS. In: Proc. The Vertical Flight Society’s, 76th Ann. Forum and Technology Display, Virtual, Oct. 5–8, 2020.
[13] Denton H., Benedict M., Kang H., Hrishikeshavan V.: Design, development and flight testing of a gun-launched rotary-wing micro air vehicle. In: Proc. The Vertical Flight Society’s, 76th Ann. Forum and Technology Display, Virtual, Oct. 5–8, 2020.
[14] Halder A., Benedict M.: Understanding upward scalability of cycloidal rotors for large-scale UAS applications. In: Proc. Aeromechanics for Advanced Vertical Flight Technical Meeting 2020, Transformative Vertical Flight 2020, San Jose, 21–23 Jan. 2020, 311–330.
[15] Runco C., Benedict M.: Flight dynamics model identification of a meso-scale twin-cyclocopter in hover. Paper presented at the 77th Ann. Vertical Flight Society Forum and Technology Display, The Future of Vertical Flight, Virtual, May 10-14, 2021.
[16] Runco C., Coleman D., Benedict M.: Design and development of a 30 g cyclocopter. J. Am. Helicopter Soc. 64(2019), 1.
[17] Coleman D., Halder A., Saemi F., Runco C., Denton H., Lee B., Benedict M.: Development of “Aria”, a compact, ultra-quiet personal electric helicopter. In: Proc. 77th Annual Vertical Flight Society Forum and Technology Display, FORUM 2021: The Future of Vertical Flight, Virtual, May 10–14, 2021.
[18] Koschorrek P., Siebert Ch., Haghani A., Jeinsch T.: Dynamic positioning with active roll reduction using Voith Schneider propeller. IFAC-PapersOnLine, 48(2015), 16, 178–183.
[19] Schubert A., Koschorrek P., Kurowski M., Lampe B., Jeinsch T.: Roll damping using Voith Schneider propeller a repetitive control approach. IFACPapersOnLine 49(2016), 23, 557–561.
[20] Hahn T., Koschorrek P., Jeinsch T.: Parameter estimation of wave-induced oscillatory ship motion for wave filtering in dynamic positioning. IFAC-PapersOnLine 51(2018), 29, 183–188.
[21] Hashem I., Mohamed M.H.: Aerodynamic performance enhancements of H-rotor Darrieus wind turbine. Energy 142(2018), 531–545
[22] Siegel S.: Numerical benchmarking study of a cycloidal wave energy converter. Renew. Energ. 134(2019), 390–405.
[23] Siegel S.: Wave radiation of a cycloidal wave energy converter. Appl. Ocean Res. 49(2015), 9–19.
[24] Bianchini A., Balduzzi F., Rainbird J., Peiro J., Graham M., Ferrara G.: An experimental and numerical assessment of airfoil polars for use in Darrieus wind turbines – Part I: Flow curvature effects. J. Eng. Gas Turb. Power 138(2016), 032602-1.
[25] Dykas S., Majkut M., Smołka K., Strozik M., Chmielniak T., Stasko T.: Numerical and experimental investigation of the fan with cycloidal rotor. Mech. Mechanical Eng. 22(2018), 2, 447–454.
[26] Stasko T., Dykas S., Majkut M., Smołka K.: An attempt to evaluate the cycloidal rotor fan performance, Open J. Fluid Dyn. 9(2019), 292–30.
[27] Shyy W., Lian Y., Tang J., Viieru D., Liu H.: Aerodynamics of Low Reynolds Flyers. Cambridge Univ. Press, 2008.
[28] Ansys Fluent User Guide 2020 R1. Ansys, Canonsburg 2020.
[29] Shrestha E., Yeo D., Benedict M., Chopra I.: Development of a meso-scale cycloidal-rotor aircraft for micro air vehicle application. Int. J. Micro Air Veh. 9(2017), 3.
[30] Augusto J., Monteiro L., Pascoa J., Xisto C.: Aerodynamic optimization of cyclorotors. Aircraft Eng. Aerosp. Tec. 88(2016), 2.
Go to article

Authors and Affiliations

Tomasz Staśko
1
Mirosław Majkut
1
Sławomir Dykas
1
Krystian Smołka
1

  1. Department of Power Engineering and Turbomachinery, Silesian University of Technology, Konarskiego 18, 44-100 Gliwice, Poland
Download PDF Download RIS Download Bibtex

Abstract

Three commercially available intercooled compression strategies for compressing CO2 were studied. All of the compression concepts required a final delivery pressure of 153 bar at the inlet to the pipeline. Then, simulations were used to determine the maximum safe pipeline distance to subsequent booster stations as a function of inlet pressure, environmental temperature, thickness of the thermal insulation and ground level heat flux conditions. The results show that subcooled liquid transport increases energy efficiency and minimises the cost of CO2 transport over long distances under heat transfer conditions. The study also found that the thermal insulation layer should not be laid on the external surface of the pipe in atmospheric conditions in Poland. The most important problems from the environmental protection point of view are rigorous and robust hazard identification which indirectly affects CO2 transportation. This paper analyses ways of reducing transport risk by means of safety valves.

Go to article

Authors and Affiliations

Mirosław Majkut
Andrzej Witkowski
Andrzej Rusin
Katarzyna Stolecka
Download PDF Download RIS Download Bibtex

Abstract

The paper presents experimental investigations of pressure fluctuations near the tip clearance region of the rotor blades of the axial-flow low-speed compressor stage in stable and unstable parts of the overall performance characteristic. In this investigation, unsteady pressure was measured with the use of high frequency pressure transducers mounted on the casing wall of rotor passage. The pressure signals and their frequency characteristics were analyzed during the steady-state processes, before the rotating stall, during the transition from the steady-state process to the rotating stall, and during a stabilized phenomenon of low-frequency rotating stall. As the operating point moves to the unstable region of flow characteristic, an inception of the rotating stall can be observed, which rotates with a speed of about 41.4% of the rotor speed. The results of this study confirm that in the low-speed axial compressor stage operating in a rotating stall regime there appears one stall cell that spreads over to adjacent rotor blade channels. As the flow rate is reduced further, the frequency of the rotating stall decreased to 34.8% of the rotor speed and the number of blade channels with the stall cell increases.

Go to article

Authors and Affiliations

Andrzej Witkowski
Marcin Ziach
Mirosław Majkut
Michał Strozik
Download PDF Download RIS Download Bibtex

Abstract

The highly dynamic and unsteady characteristics of the cavitating flow cause many negative effects such as erosion, noise and vibration. Also, in the real application, it is inevitable to neglect the dissolved air in the water, although it is usually neglected in the previous works to reduce the complexity. The novelty of the present work is analysing the impact of dissolved air on the average/unsteady characteristics of Venturi flow by conducting sets of experimental tests. For this purpose, two different amounts of dissolved air at five pressure levels (i.e. five different sets of cavitation numbers) were considered in the study of cavitating flow inside a Venturi nozzle. The fast Fourier transform analysis of pressure fluctuations proved that the shedding frequency reduces almost by 50% to 66%, depending on the case, with adding the amount of dissolved air. However, the reduction of 14% to 25% is achieved by the vibration transducers. On the other hand, the cavity enlarges as well as bubbly flow is observed in the test chamber at a higher level of dissolved air. Furthermore, it is observed that the re-entrant jet, as the main reason for the cavity detachment, is more effective for the detachment process in cases with a lower level of dissolved air, where the re-entrant jet front penetrates more toward the leading edge.
Go to article

Authors and Affiliations

Emad Hasani Malekshah
1
Włodzimierz Wróblewski
1
Krzysztof Bochon
1
Mirosław Majkut
1
Krzysztof Rusin
1

  1. Silesian University of Technology, Department of Power Engineering and Turbomachinery, Konarskiego 18, 44-100 Gliwice, Poland
Download PDF Download RIS Download Bibtex

Abstract

Besides centrifugal pumps, centrifugal fans are the most common turbomachines used in technical applications. They are commonly used in power engineering systems, such as heat engines and chillers, heating, ventilation, and air conditioning systems, supply and exhaust air systems. They are also used as machines consuming final energy (electricity). Therefore, any improvement in their efficiency affects the efficiency of energy generation and the level of electricity consumption. Many efforts have been made so far to find the most efficient numerical method of modelling flows in fans. However, only a few publications focus on the unsteadiness that may have an impact on device efficiency and noise generation. This paper presents an attempt to identify unsteadiness in the flow through a centrifugal fan by means of computational fluid dynamics and computational aeroacoustics methods. The works were performed using the Ansys CFX commercial software and the results of numerical studies are compared with experimental data.
Go to article

Bibliography

[1] Dykas S., Wróblewski W., Rulik S., Chmielniak T.: Numerical method for modelling of acoustic waves propagation. Arch. Acoust. 35(2010), 1, 35–48.
[2] Fortuna S., Sobczak K.: Numerical and experimental investigations of the flow in radial fan. Mechanics 27(2008), 4, 138–143
[3] Moon Y.J., Cho Y., Nam H.S.: Computation of unsteady viscous flow and aeroacoustic noise of the cross flow fan. Comput. Fluids 32(2003), 7, 995–1015.
[4] Rulik S., Dykas S., Wroblewski W.: Modelling of aerodynamic noise using hybrid SAS and DES methods. In: Proc. ASME Turbo Expo 2010: Power for Land, Sea and Air, Glasgow, June 14–18, 2010, 7(2010), 2835–2844., GT2010-2269.
[5] Stasko T., Dykas S., Majkut M., Smolka K.: An attempt to evaluate the cycloidal rotor fan performance. Open J. Fluid Dynam. 9(2019), 4.
[6] Benedek T., Vad J.: Beamforming based extension of semi-empirical noise modelling for low-speed axial flow fans. Appl. Acoust. 178(2021), 108018.
[7] Jiang H., Wang Q., Zheng T.F., Tu C.X., Zhang K.: PIV measurement of internal flow field in a range hood. In: Energy and Mechanical Engineering (S.Y. Liang, Ed.), 2015 Int. Conf. on Energy and Mechanical Engineering, Wuhan, 17-18 Oct. 2015, World Scientific, 2016, 570–575.
[8] Probst M., Pritz B.: Quantitative validation of CFD-simulation against PIV data for a centrifugal fan. In: Proc. 14th Int. Symp. on Experimental Computational Aerothermodynamics of Internal Flows, Gdansk 8-11 July 2019.
[9] Neise W., Michel U.: Aerodynamic Noise of Turbomachines. DLR-Interner Bericht, Berlin 1994.
[10] Jeon W.H., Lee D.J., Rhee H.: An application of the acoustic similarity law to the numerical analysis of centrifugal fan noise. JSME Int. J. C-mech Sy. 47(2004), 3, 845–851.
[11] Kissner C., Guerin S.: Comparison of predicted fan broadband noise using a twoversus a three-dimensional synthetic turbulence method. J. Sound Vib. 508(2021), 116221.
[12] Jaron R., Herthum H., Franke M., Moreau A., Guerin S.: Impact of turbulence models on RANS-informed prediction of fan broadband interaction noise. In: Proc. 12th Eur. Turbomachinery Conference (ETC), Stockholm, 3-7 April, 2017.
[13] Carolus T.: Theoretische und experimentelle Untersuchung des Pumpens von lufttechnischen Anlagen mit Radialventilatoren. PhD thesis, Karlsruhe University of Applied Sciences, Karlsruhe 1984.
[14] Blazquez-Navarro R., Corral R.: Prediction of fan acoustic blockage on fan/outlet guide vane broadband interaction noise using frequency domain linearized Navier–Stokes solvers. J. Sound Vib. 508(2021), 116033.
[15] Ffowcs-Williams J.E., Hawkings D.L.: Sound generation by turbulence and surfaces in arbitrary motion. Philos. T.R. Soc. Lond. S-A, 264(1969), 1151, 321–342.
[16] Lighthill M.J.: On sound generated aerodynamically. I. General theory. Proc. R. Soc. Lon. Ser.-A 211(1952) 1107, 564–587
[17] Menter F.R., Egorov Y.: A scale-adaptive simulation model using two-equation models. In: Proc. 43th AIAA Aerospace Sciences Meeting and Exhibit, Reno, 10-13 Jan. 2005, AIAA 2005-1095.
[18] Ansys Fluent Theory Guide, 2021R1. https://www.ansys.com (acessed 1 July 12021).
Go to article

Authors and Affiliations

Balazs Pritz
1
Matthias Probst
1
Piotr Wiśniewski
2
Sławomir Dykas
2
Mirosław Majkut
2
Krystian Smołka
2

  1. Institute of Thermal Turbomachinery, Karlsruhe Institute of Technology, Kaiserstraße 12 D-76131 Karlsruhe, Germany
  2. Department of Power Engineering and Turbomachinery, Silesian University of Technology, Poland

This page uses 'cookies'. Learn more