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2019

Effects of upstream bend on aerodynamic performance of a transonic centrifugal compressor

Yamada, K., Furukawa, M., Arai, H. & Ito, S., Jan 1 2019, Turbomachinery. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 2B-2019).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Centrifugal compressors
Aerodynamics
Pipe
Compressors
Flow rate

Mechanisms and quantitative evaluation of flow loss generation in a multi-stage transonic axial compressor

Saito, S., Furukawa, M., Yamada, K., Watanabe, K., Matsuoka, A. & Niwa, N., Jan 1 2019, Turbomachinery. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 2A-2019).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Compressors
Vortex flow
Flow fields
Boundary layers
Shock waves

Simultaneous optimization of impeller blade loading distribution and meridional geometry for aerodynamic design of centrifugal compressor

Manabe, K., Ito, S., Furukawa, M., Yamada, K., Oka, N., Tomita, I. & Hayashi, Y., Jan 1 2019, Fluid Applications and Systems. American Society of Mechanical Engineers (ASME), 5358. (ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019; vol. 3A-2019).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Centrifugal compressors
Aerodynamics
Viscous flow
Geometry
Flow fields

Suppression of secondary flows in a transonic centrifugal compressor impeller using an inverse design method based on meridional viscous flow analysis

Ito, S., Okada, S., Kawakami, Y., Manabe, K., Furukawa, M. & Yamada, K., Jan 1 2019, Fluid Applications and Systems. American Society of Mechanical Engineers (ASME), 5319. (ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019; vol. 3A-2019).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Centrifugal compressors
Secondary flow
Viscous flow
Impellers
Vortex flow
2017
1 Citation (Scopus)

A study on unsteady flow phenomena at near-stall in a multi-stage axial flow compressor by large-scale DES with K computer

Yamada, K., Furukawa, M., Nakakido, S., Tamura, Y., Matsuoka, A. & Nakayama, K., Feb 1 2017, In : International Journal of Gas Turbine, Propulsion and Power Systems. 9, 1, p. 18-26 9 p.

Research output: Contribution to journalArticle

Axial-flow compressors
Unsteady flow
Compressors
Large eddy simulation
Gas turbines
3 Citations (Scopus)

Evolution of reverse flow in a transonic centrifugal compressor at near-surge

Yamada, K., Furukawa, M., Arai, H. & Kanzaki, D., Jan 1 2017, Turbomachinery. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 2C-2017).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Centrifugal compressors
Flow fields
Compressors
Unsteady flow
8 Citations (Scopus)

Large-scale detached-eddy simulation analysis of stall inception process in a multistage axial flow compressor

Yamada, K., Furukawa, M., Tamura, Y., Saito, S., Matsuoka, A. & Nakayama, K., Jul 1 2017, In : Journal of Turbomachinery. 139, 7, 071002.

Research output: Contribution to journalArticle

Axial-flow compressors
Compressors
Large eddy simulation
Stators
Gas turbines
3 Citations (Scopus)

Optimum aerodynamic design of centrifugal compressor impeller using an inverse method based on meridional viscous flow analysis

Oka, N., Furukawa, M., Yamada, K., Itou, S., Ibaraki, S., Iwakiri, K. & Hayashi, Y., Jan 1 2017, Turbomachinery. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 2C-2017).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Centrifugal compressors
Viscous flow
Aerodynamics
Flow fields
Flow separation
2 Citations (Scopus)

Optimum aerodynamic design of centrifugal comPressor using a genetic algorithm and an inverse method based on meridional viscous flow analysis

Itou, S., Oka, N., Furukawa, M., Yamada, K., Ibaraki, S., Iwakiri, K. & Hayashi, Y., Jan 1 2017.

Research output: Contribution to conferencePaper

Centrifugal compressors
Viscous flow
Aerodynamics
Genetic algorithms
Flow fields
3 Citations (Scopus)

Study on influence of blade number on aerodynamic noise of half-ducted propeller fans for packaged air-conditioners

Iwase, T., Kishitani, T. & Furukawa, M., Oct 1 2017, In : International Journal of Fluid Machinery and Systems. 10, 4, p. 318-327 10 p., O16044C.

Research output: Contribution to journalArticle

Propellers
Fans
Aerodynamics
Air
Vortex flow
1 Citation (Scopus)

Vortical flow structure of hub-corner separation in a stator cascade of a multi-stage transonic axial compressor

Saito, S., Furukawa, M., Yamada, K., Tamura, Y., Matsuoka, A. & Niwa, N., 2017, Symposia: Keynotes; Advances in Numerical Modeling for Turbomachinery Flow Optimization; Fluid Machinery; Industrial and Environmental Applications of Fluid Mechanics; Pumping Machinery. American Society of Mechanical Engineers (ASME), Vol. 1A-2017.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Flow structure
Stators
Compressors
Vortex flow
Flow fields
2016
1 Citation (Scopus)

Direct numerical simulation of turbulent flow and aeroacoustic fields around an airfoil using lattice boltzmann method

Kusano, K., Yamada, K., Furukawa, M. & Moon, K. J., Jan 1 2016, Symposia: Turbomachinery Flow Simulation and Optimization; Applications in CFD; Bio-Inspired and Bio-Medical Fluid Mechanics; CFD Verification and Validation; Development and Applications of Immersed Boundary Methods; DNS, LES and Hybrid RANS/LES Methods; Fluid Machinery; Fluid-Structure Interaction and Flow-Induced Noise in Industrial Applications; Flow Applications in Aerospace; Active Fluid Dynamics and Flow Control - Theory, Experiments and Implementation. American Society of Mechanical Engineers (ASME), (American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FEDSM; vol. 1A-2016).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Aeroacoustics
Direct numerical simulation
Airfoils
Turbulent flow
Boundary layers
2 Citations (Scopus)

Large-scale des analysis of stall inception process in a multi-stage axial flow compressor

Yamada, K., Furukawa, M., Tamura, Y., Saito, S., Matsuoka, A. & Nakayama, K., Jan 1 2016, Turbomachinery. American Society of Mechanical Engineers (ASME), Vol. 2D-2016.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Axial-flow compressors
Compressors
Stators
Gas turbines
Unsteady flow
2015

Aerodynamic performances and flow fields of pareto optimal solutions in an aerodynamic design of a wind-lens turbine

Oka, N., Furukawa, M., Yamada, K., Oka, A. & Kurokawa, Y., Jan 1 2015, Oil and Gas Applications; Supercritical CO2 Power Cycles; Wind Energy. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 9).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Lenses
Flow fields
Aerodynamics
Turbines
Wind turbines
1 Citation (Scopus)

Effects of flow path height of impeller exit and diffuser on flow fields in a transonic centrifugal compressor

Tomita, I., Ibaraki, S., Wakashima, K., Furukawa, M., Yamada, K. & Kanzaki, D., Jan 1 2015, Turbomachinery. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 2C).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Centrifugal compressors
Flow fields
Electric inductors
Unsteady flow
Momentum
9 Citations (Scopus)

Large-scale des analysis of unsteady flow field in a multi-stage axial flow compreßor at off-design condition using k computer

Yamada, K., Furukawa, M., Nakakido, S., Matsuoka, A. & Nakayama, K., Jan 1 2015, Turbomachinery. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 2C).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Axial flow
Unsteady flow
Flow fields
Boundary conditions
Gas turbines

Large-scale numerical simulation of unsteady flow field in a half-ducted propeller fan using lattice Boltzmann method

Yamada, K., Kusano, K. & Furukawa, M., Jan 1 2015.

Research output: Contribution to conferencePaper

Acoustic fields
Propellers
Unsteady flow
Fans
Flow fields

Measurement technique for unsteady low-speed flow fields using poly(TMSP)-based pressure sensitive paint

Mori, H., Maeda, K., Furukawa, M. & Akiyoshi, M., Jan 1 2015.

Research output: Contribution to conferencePaper

Paint
Flow fields
Polymers
Oxygen
Quenching

Numerical analysis of unsteady three-dimensional flow in a propeller fan using multi-scale lattice boltzmann method

Kusano, K., Yamada, K. & Furukawa, M., Jan 1 2015, FAN 2015 - International Conference on Fan Noise, Technology and Numerical Methods. Institution of Mechanical Engineers, Vol. 2015-April.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

propeller fans
three dimensional flow
numerical analysis
simulation
computational grids
2014
4 Citations (Scopus)

Simultaneous optimization of rotor blade and wind-lens for aerodynamic design of wind-lens turbine

Oka, N., Furukawa, M., Yamada, K., Kawamitsu, K., Kido, K. & Oka, A., Jan 1 2014, ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, GT 2014. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 3B).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Turbomachine blades
Lenses
Aerodynamics
Turbines
Rotors
1 Citation (Scopus)

Suppression of secondary flows in an axial flow turbine rotor with a novel blade design concept

Yamada, K., Furukawa, M., Shibata, T., Nakakido, S. & Oka, N., Jan 1 2014, Turbomachinery. American Society of Mechanical Engineers (ASME), (Proceedings of the ASME Turbo Expo; vol. 2C).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Cambers
Axial flow
Secondary flow
Turbomachine blades
Turbines
2013
6 Citations (Scopus)

Aerodynamic design for wind-lens turbine using optimization technique

Oka, N., Furukawa, M., Yamada, K. & Kido, K., Dec 1 2013, ASME 2013 Fluids Engineering Division Summer Meeting, FEDSM 2013. V01AT02A009. (American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FEDSM; vol. 1 A).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Lenses
Aerodynamics
Turbines
Rotors
Viscous flow
1 Citation (Scopus)

Effects of tip clearance flow on rotating stall inception process in an axial compressor rotor

Yamada, K., Kikuta, H., Furukawa, M., Gunjishima, S. & Hara, Y., Jul 15 2013, In : Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B. 79, 801, p. 900-916 17 p.

Research output: Contribution to journalArticle

compressor rotors
rotating stalls
turbocompressors
clearances
Compressors
25 Citations (Scopus)

Effects of tip clearance on the stall inception process in an axial compressor rotor

Yamada, K., Kikuta, H., Furukawa, M., Gunjishima, S. & Hara, Y., Dec 17 2013, ASME Turbo Expo 2013: Turbine Technical Conference and Exposition, GT 2013. GT2013-95479. (Proceedings of the ASME Turbo Expo; vol. 6 C).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Compressors
Vortex flow
Rotors
Flow fields
Tornadoes
16 Citations (Scopus)

The effect of tip leakage vortex for operating range enhancement of centrifugal compressor

Tomita, I., Ibaraki, S., Furukawa, M. & Yamada, K., Jun 28 2013, In : Journal of Turbomachinery. 135, 3, 051020.

Research output: Contribution to journalArticle

Centrifugal compressors
Compressors
Vortex flow
Flow rate
Flow structure
1 Citation (Scopus)

Toward direct numerical simulation of aeroacoustic field around airfoil using multi-scale lattice boltzmann method

Kusano, K., Yamada, K. & Furukawa, M., Dec 1 2013, ASME 2013 Fluids Engineering Division Summer Meeting, FEDSM 2013. V01AT09A005. (American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FEDSM; vol. 1 A).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Aeroacoustics
Direct numerical simulation
Airfoils
Mach number
Flow fields
2012
6 Citations (Scopus)

An explanation for flow features of spike-type stall inception in an axial compressor rotor

Yamada, K., Kikuta, H., Iwakiri, K. I., Furukawa, M. & Gunjishima, S., Dec 1 2012, ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A, B, AND C ed. p. 2663-2675 13 p. (Proceedings of the ASME Turbo Expo; vol. 8, no. PARTS A, B, AND C).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Compressors
Rotors
Tornadoes
Vortex flow
Flow structure
70 Citations (Scopus)

An Explanation for Flow Features of Spike-Type Stall Inception in an Axial Compressor Rotor

Yamada, K., Kikuta, H., Iwakiri, K. I., Furukawa, M. & Gunjishima, S., Nov 5 2012, In : Journal of Turbomachinery. 135, 2, 021023.

Research output: Contribution to journalArticle

Compressors
Rotors
Tornadoes
Vortex flow
Flow structure
3 Citations (Scopus)

Development of advanced centrifugal compressor for turbocharger, applying control of internal unsteady flow structure

Ebisu, M., Shiraishi, T., Tomita, I. & Furukawa, M., Jan 1 2012, Institution of Mechanical Engineers - 10th International Conference on Turbochargers and Turbocharging. Woodhead Publishing Limited, p. 135-144 10 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Centrifugal compressors
Flow structure
Unsteady flow
Compressors
Exhaust gases
3 Citations (Scopus)

The effect of tip leakage vortex for operating range enhancement of centrifugal compressor

Tomita, I., Ibaraki, S., Furukawa, M. & Yamada, K., Dec 1 2012, ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A, B, AND C ed. p. 735-743 9 p. (Proceedings of the ASME Turbo Expo; vol. 8, no. PARTS A, B, AND C).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Centrifugal compressors
Compressors
Vortex flow
Flow rate
Flow structure
2011

Circulation of a vortex ring generated by pulsating jet flow

Akagi, F., Kawabata, K., Ando, Y., Yamaguchi, S. & Furukawa, M., Dec 1 2011, ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011. PARTS A, B, C, D ed. p. 2911-2920 10 p. (ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011; vol. 1, no. PARTS A, B, C, D).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Vortex flow
Strouhal number
Measurement errors
Momentum
5 Citations (Scopus)

Detached eddy simulation of unsteady flow field and prediction of aerodynamic sound in a half-ducted propeller fan

Kusano, K., Jeong, J. H., Yamada, K. & Furukawa, M., Dec 1 2011, ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011. PARTS A, B, C, D ed. p. 713-722 10 p. (ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011; vol. 1, no. PARTS A, B, C, D).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Propellers
Unsteady flow
Fans
Flow fields
Aerodynamics
2 Citations (Scopus)

Formation process of vortex ring generated by a pulsating jet flow

Akagi, F., Okuzono, Y., Ando, Y., Yamaguchi, S. & Furukawa, M., Dec 1 2011, In : Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B. 77, 775, p. 546-556 11 p.

Research output: Contribution to journalArticle

vortex rings
jet flow
Vortex flow
nozzles
Nozzles
axial flow
casing
Axial flow
Noise abatement
blades
8 Citations (Scopus)

The role of tip leakage vortex breakdown in flow fields and aerodynamic characteristics of transonic centrifugal compressor impellers

Yamada, K., Furukawa, M., Fukushima, H., Ibaraki, S. & Tomita, I., Dec 1 2011, ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011. PARTS A, B, AND C ed. p. 2111-2123 13 p. (Proceedings of the ASME Turbo Expo; vol. 7, no. PARTS A, B, AND C).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Impellers
Centrifugal compressors
Flow fields
Aerodynamics
Vortex flow
6 Citations (Scopus)

Unsteady and three-dimensional flow mechanism of spike-type stall inception in an axial flow compressor rotor

Kikuta, H., Iwakiri, K. I., Furukawa, M., Yamada, K., Gunjishima, S. & Okada, G., Dec 1 2011, ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011. PARTS A, B, C, D ed. p. 817-829 13 p. (ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011; vol. 1, no. PARTS A, B, C, D).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Axial-flow compressors
Vortex flow
Rotors
Flow structure
Tornadoes
2010
11 Citations (Scopus)

Comparative study on tip clearance flow fields in two types of transonic centrifugal compressor impeller with splitter blades

Yamada, K., Tamagawa, Y., Fukushima, H., Furukawa, M., Ibaraki, S. & Iwakiri, K. I., Dec 1 2010, ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010. PARTS A, B, AND C ed. p. 2053-2063 11 p. (Proceedings of the ASME Turbo Expo; vol. 7, no. PARTS A, B, AND C).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Centrifugal compressors
Turbomachine blades
Compressors
Flow fields
Vortex flow