九州大学 研究者情報
論文一覧
山田 和豊(やまだ かずとよ) データ更新日:2017.05.24

助教 /  工学研究院 機械工学部門 流体工学


原著論文
1. Kazutoyo Yamada, Masato Furukawa, Satoshi Nakakido, Yuki Tamura, Akinori Matsuoka, Kentaro Nakayama, A Study on Unsteady Flow Phenomena at Near-Stall in a Multi-Stage Axial Flow Compressor by Large-Scale DES with K Computer, International Journal of Gas Turbine, Propulsion and Power Systems, 9, 1, 2017.02.
2. Kazutoyo Yamada, Masato Furukawa, Yuki Tamura, Seishiro Saito, Akinori Matsuoka, Kentaro Nakayama, Large-Scale Detached-Eddy Simulation Analysis of Stall Inception Process in a Multi-Stage Axial Flow Compressor, ASME, Journal of Turbomachinery, 139, 7, 071002-1-071002-11, 2017.02.
3. Kazuya Kusano, Kazutoyo Yamada, Masato Furukawa, Kil-Ju Moon, Direct Numerical Simulation of Turbulent Flow and Aeroacoustic Fields around an Airfoil Using Lattice Boltzmann Method, ASME FEDSM 2016, FEDSM2016-7585, 2016.07.
4. Nobuhito Oka, Masato Furukawa, Kentaro Kawamitsu, Kazutoyo Yamada, Optimum Aerodynamic Design for Wind-Lens Turbine, Journal of Fluid Science and Technology, 11, 2, 2016.06.
5. Kazutoyo Yamada, Masato Furukawa, Yuki Tamura, Seishiro Saito, Akinori Matsuoka, Kentaro Nakayama, Large-Scale DES Analysis of Stall Inception Process in a Multi-Stage Axial Flow Compressor, ASME Turbo Expo 2016, GT2016-57104, 2016.06.
6. Kazutoyo Yamada, Masato Furukawa, Satoshi Nakakido, Yuki Tamura, Akinori Matsuoka, Kentaro Nakayama, A Study on Unsteady Flow Phenomena at Near-Stall in a Multi-Stage Axial Flow Compressor by Large-Scale DES with K Computer, IGTC2015 Tokyo, 2015.11.
7. Nobuhito Oka, Masato Furukawa, Kazutoyo Yamada, Yuki Tamura, Shoji Yamada, Takahide Tadokoro, Naohiko Honma, Improvement in Aerodynamic Performance of a Half-Ducted Axial Flow Fan using Meridional Viscous Flow Analysis, The 13th Asian International Conference on Fluid Machinery (AICFM13), AICFM13-073, 2015.09.
8. Kazutoyo Yamada, Kazuya Kusano, Masato Furukawa, Large-Scale Numerical Simulation of Unsteady Flow Field in a Half-Ducted Propeller Fan Using Lattice Boltzmann Method, AJK2015-FED, AJK2015-09494, 2015.07.
9. Kazutoyo Yamada, Masato Furukawa, Satoshi Nakakido, Akinori Matsuoka, Kentaro Nakayama, Large-Scale DES Analysis of Unsteady Flow Field in a Multi-Stage Axial Flow Compressor at Off-Design Condition Using K Computer, ASME Turbo Expo 2015, GT2015-42648, 2015.06.
10. Isao Tomita, Sei-ichi Ibaraki, Masato Furukawa, Kazutoyo Yamada, Dai Kanzaki, Koji Wakashima, Effects of Flow Path Height of Impeller Exit and Diffuser on Flow Fields in a Transonic Centrifugal Compressor, ASME Turbo Expo 2015, GT2015-43271, 2015.06.
11. Nobuhito Oka, Masato Furukawa, Kazutoyo Yamada, Akihiro Oka, Yasushi Kurokawa, Aerodynamic Performances and Flow Fields of Pareto Optimal Solutions in an Aerodynamic Design of a Wind-Lens Turbine, ASME Turbo Expo 2015, GT2015-43619, 2015.06.
12. Kazuya Kusano, Kazutoyo Yamada, Masato Furukawa, Numerical Analysis of Unsteady Three-Dimensional Flow in a Propeller Fan Using Lattice Boltzmann Method, Fan2015, 2015.04.
13. Nobuhito Oka, Kota Kido, Kazutoyo Yamada, Masato Furukawa, Aerodynamic Design of Wind-Lens Turbine with Axisymmetric Viscous Flow Calculation using Lattice Boltzmann Method, 5th Asian Joint Workshop on Thermophysics and Fluid Science, 2014.09.
14. Kazutoyo Yamada, Masato Furukawa, Takanori Shibata, Satoshi Nakakido, Nobuhito Oka, Suppression of Secondary Flows in an Axial Flow Turbine Rotor With a Novel Blade Design Concept, ASME Turbo Expo 2014, GT2014-25630, 2014.06.
15. Nobuhito Oka, Masato Furukawa, Kazutoyo Yamada, Kenta Kawamitsu, Kota Kido, Akihiro Oka, Simultaneous Optimization of Rotor Blade and Wind-Lens for Aerodynamic Design of Wind-Lens Turbine, ASME Turbo Expo 2014, GT2014-25770, 2014.06.
16. 草野 和也, 古川 雅人, 山田 和豊, 半開放形プロペラファンにおける翼端渦の三次元構造, 日本機械学会論文集, 80, 810, 1-17, 2014.02.
17. Nobuhito Oka, Masato Furukawa, Kazutoyo Yamada, Kenta Kawamitsu, Kota Kido, Akihiro Oka, Aerodynamic Design Optimization of Wind-lens Turbine, EWEA2014, PO.ID210, 2014.03.
18. 草野 和也, 山田 和豊, 古川 雅人, 半開放形プロペラファンにおける翼端渦の三次元構造, 日本機械学会論文集, 80, 810, 2014.02.
19. Isao Tomita, Seiichi Ibaraki, Masato Furukawa, Kazutoyo Yamada, The Effect of Tip Leakage Vortex for Operating Range Enhancement of Centrifugal Compressor, ASME J. Turbomach., 135, 5, 051020-1-051020-8, GT2012-68947, 2013.09.
20. Kazuya Kusano, Kazutoyo Yamada, Masato Furukawa, Toward Direct Numerical Simulation of Aeroacoustic Field around Airfoil Using Multi-Scale Lattice Boltzmann Method, ASME FEDSM 2013, FEDSM2013-16526, 2013.07.
21. Nobuhito Oka, Masato Furukawa, Kazutoyo Yamada, Kota Kido, Aerodynamic Design for Wind-Lens Turbine Using Optimization Technique, ASME FEDSM 2013, FEDSM2013-16569, 2013.07.
22. Kazutoyo Yamada, Hiroaki Kikuta, Masato Furukawa, Satoshi Gunjishima, Yasunori Hara, Effects of Tip Clearance on the Stall Inception Process in an Axial Compressor Rotor, ASME Turbo Expo 2013, GT2013-95479, 2013.06.
23. 山田 和豊, 喜久田 啓明, 古川 雅人, 郡司嶋 智, 原 靖典, 軸流圧縮機動翼列における旋回失速初生プロセスに及ぼす翼端すき間流れの影響, 日本機械学会論文集B編, 79, 801, 900-916, 2013.05.
24. Kazutoyo Yamada, Hiroaki Kikuta, Kenichiro Iwakiri, Masato Furukawa, Satoshi Gunjishima, An Explanation for Flow Features of Spike-Type Stall Inception in an Axial Compressor Rotor, ASME, J. Turbomach., 135, 2, 021023-1-021023-11, 2013.03.
25. Yamada, K., Kikuta, H., Furukawa, M., Gunjishima, S., Effects of Tip Leakage Vortex Breakdown on Unsteady Flow Fields at Near-Stall Condition in a Low-Speed Axial Flow Compressor Rotor with Large Tip Clearance, IGTC'11 Osaka, IGTC2011-56, 2011.11.
26. I. Tomita, S. Ibaraki, M. Furukawa, K. Yamada, Feature of Internal Flow Phenomena of Centrifugal Compressor for Turbocharger with Wide Operating Range, IGTC'11 Osaka, IGTC2011-0080, 2011.11.
27. K. Kusano, J. Jeong, K. Yamada and M. Furukawa, Detached Eddy Simulation of Unsteady Flow Field and Prediction of Aerodynamic Sound in a Half-Ducted Propeller Fan, AJK2011-FED, AJK2011-22048, 2011.07.
28. H. Kikuta, K. Iwakiri, M. Furukawa, K. Yamada, S. Gunjishima and G. Okada, Unsteady and Three-Dimensional Flow Mechanism of Spike-Type Stall Inception in an Axial Flow Compressor Rotor, AJK2011-FED, AJK2011-22079, 2011.07.
29. 山田和豊,古川雅人,福島久剛,茨木誠一, スプリッタ付遠心圧縮機インペラの非設計点における剥離渦流れ構造, ターボ機械, 39, 6, 332-339, 2011.06.
30. 船崎健一,高橋友恵,谷口英夫,山田和豊, 狭隘場におけるPC用冷却ファンの非定常流れ場解析(騒音との相関に関する考察), ターボ機械, 39, 2, 79-86, 2011.02.
31. Yamada, K., Furukawa, M., Fukushima, H., Ibaraki, S. and Tomita, I., The Role of Tip Leakage Vortex Breakdown in Flow Fields and Aerodynamiec Characteristics of Transonic Centrifugal Compressor Impellers, ASME Turbo Expo 2011, GT2011-46253, 2010.06.
32. 船崎健一, 山田和豊, 菊池 護, 佐藤英明, タービン段における空力特性に与える動静翼間距離の効果に関する研究(実験及び簡易モデルによるCFD), ターボ機械, 第38巻第6号,pp. 334-344, 2010.06.
33. Yamada, K., Tamagawa, Y., Fukushima, H., Furukawa, M., Ibaraki, S. and Iwakiri, K., Comparative Study on Tip Clearance Flow Fields in Two Types of Transonic Centrifugal Compressor Impeller with Splitter Blades, ASME Turbo Expo 2010, GT2010-23345, 2010.06.
34. 船崎健一, 山田和豊, 田中 望, 千葉康弘, 航空エンジン用高負荷低圧タービン翼面上剥離境界層に与える主流乱れの効果に関する研究, 日本ガスタービン学会誌, 38, 2, 115-122, 2010.03.
35. 石川慶拓, 船崎健一, 山田和豊, 高レイノルズ数条件下における高圧タービン翼まわりの非定常流れ解析(後縁近傍の非定常流れとベース圧), 日本ガスタービン学会誌, 38, 1, 50-68, 2010.01.
36. Most. Nasrin AKHTER, Kazutoyo YAMADA and Ken-ichi FUNAZAKI, Numerical Simulation of Bypass Transition by the Approach of Intermittency Transport Equation, Journal of Fluid Science and Technology, Vol. 4, No. 3, pp. 524-535, 2009.07.
37. Yamada, K., Funazaki, K., Kikuchi, M. and Sato, H., Influences of Axial Gap between Blade Rows on Secondary Flows and Aerodynamic Performance in a Turbine Stage, ASME Turbo Expo 2009, ASME GT2009-59855, 2009.06.
38. Funazaki, K., Yamada, K., Tanaka, N., and Chiba, Y., Detailed Studies on Separated Boundary Layers over Low-Pressure Turbine Airfoils under Several High Lift Conditions: Effect of Freestream Turbulence, ASME Turbo Expo 2009, ASME GT2009-59813, 2009.06.
39. 袁紅斌,船崎健一,山田和豊,島田崇史, 狭隘環境下での冷却ファンの熱流体特性(時間平均特性に関する実験と数値解析), ターボ機械, 第36巻第6号,pp. 49-57, 2008.06.
40. Yamada, K., Funazaki, K. and Sasaki, H., Numerical Investigation of Relation Between Unsteady Behavior of Tip Leakage Vortex and Rotating Disturbance in a Transonic Axial Compressor Rotor, ASME Turbo Expo 2008, GT2008-50779, 2008.06.
41. Funazaki, K., Yamada, K., Chiba, Y., and Tanaka, N., Numerical and Experimental Studies on Separated Boundary Layers Over Ultra-High Lift Low-Pressure Turbine Cascade Airfoils With Variable Solidity: Effects of Free-Stream Turbulence, ASME Turbo Expo 2008, GT2008-50718, 2008.06.
42. 船﨑健一,田中 望,小野隆浩,山田和豊,菊池 護,谷口英夫, 航空エンジン用低圧タービンの高負荷化に関する研究(wake通過時の剥離を伴う翼面境界層の動的挙動の時間平均的理解), 日本機械学会論文集B編, 74巻741号,pp. 1040-1048, 2008.05.
43. Yamada, K., Funazaki, K., and Furukawa, M., Effect of Tip Clearance on Near-Stall Flow in a Transonic Axial Compressor Rotor, International Gas Turbine Congress 2007 Tokyo, TS-045, 2007.12.
44. Kikuchi, M., Funazaki, K., Yamada, K., and Sato, H., Detailed Studies on Aerodynamic Performance and Unsteady Flow Behaviors of a Single Turbine Stage with Variable Rotor-Stator Axial Gap, International Gas Turbine Congress 2007 Tokyo, TS-067, 2007.12.
45. Ishikawa, Y., Funazaki, K., and Yamada, K., Numerical Studies on the Relationship between Base Pressure and Vortex Shedding from the Trailing Edge of a Turbine Vane, International Gas Turbine Congress 2007 Tokyo, TS-083, 2007.12.
46. Funazaki, K., Yamada, K., Kikuchi, M. and Sato, H., Experimental Studies on Aerodynamic Performance and Unsteady Flow Behaviors of a Single Turbine Stage with Variable Rotor-Stator Axial Gap: Comparisons with Time-Accurate Numerical Simulation, ASME Turbo Expo 2007, GT2007-20670, 2007.05.
47. Yamada, K., Funazaki, K. and Furukawa, M., The Behavior of Tip Clearance Flow at Near-Stall Condition in a Transonic Axial Compressor Rotor, ASME Turbo Expo 2007, GT2007-27725, 2007.05.
48. 船崎健一,東正浩,山田和豊,谷口英夫,戸村則昭, リアル形状の脳動脈瘤を有する脳動脈の流体-構造連成解析, 日本機械学会論文集B編, 73巻731号,pp.1472-1479, 2007.03.
49. 船崎健一,山田和豊,中村豪, 動脈瘤を伴う脳動脈分岐部まわりの非ニュートン流体解析, 日本機械学会論文集B編, 72巻713号, pp. 1-8, 2006.12.
50. 船崎健一,山田和豊,佐藤浩平, 遺伝的アルゴリズムによる複合型インピンジメント冷却構造の最適化, 日本ガスタービン学会誌, Vol.34, No. 6, pp. 439-445, 2006.11.
51. Funazaki, K., Yamada, K., Ono, T., Segawa, K., Hamazaki, H., Takahashi, A., and Tanimitsu, H., Experimental and Numerical Investigations of Wake Passing Effects upon Aerodynamic Performance of a LP Turbine Linear Cascade With Variable Solidity, ASME Turbo Expo 2006, GT2006-90507, 2006.05.
52. Yamada, K., Funazaki, K., Hiroma, K., Tsutsumi, M., Hirano, Y., and Matsuo, A., Effect Of Wake Passing On Unsteady Aerodynamic Performance in a Turbine Stage, ASME Turbo Expo 2006, GT2006-90783, 2006.05.
53. 山田和豊,船崎健一,廣間和人,堤雅徳,平野雄一郎,松尾淳, タービン性能に及ぼす動静翼間距離の効果, 日本機械学会論文集B編, 72巻716号,pp. 933-941, 2006.04.
54. Yamada, K., Furukawa, M., Inoue, M., Funazaki, K., Numerical Analysis of Tip Leakage Flow Field in a Transonic Axial Compressor Rotor, 日本ガスタービン学会誌, Vol. 34, No. 2, pp.124-132, 2006.03.
55. Iwakiri, K., Furukawa, M., Tomita, I., Yamada, K., and Kuroumaru, M., Vortical Flow Field in an Axial Flow Compressor Rotor at Rotating Stall Inception, the 3rd International Conference on Vortex Flows and Vortex Models, pp. 211-216, 2005.11.
56. 船崎健一,山田和豊,Favaretto Carlos Felipe F.,田沼唯士, 遺伝的アルゴリズムによる蒸気注入用スワーラーの最適設計, 日本ガスタービン学会誌, Vol.33,No.4,pp.343-351, 2005.07.
57. Funazaki, K., Yamada, K., Kato, Y., Studies on Effects of Periodic Wake Passing upon a Blade Leading Edge Separation Bubble: Suppresion of Separation Bubble Due to Wake Passing, JSME international journal. Ser. B, Fluids and thermal engineering, Vol.47, No.3, pp.612-621, 2004.08.
58. Yamada, K., Furukawa, M., Nakano, T., Inoue, M., and Funazaki, K., Unsteady Three-Dimensional Flow Phenomena Due to Breakdown of Tip Leakage Vortex in a Transonic Axial Compressor Rotor, ASME Turbo Expo 2004, GT2004-53745, 2004.06.
59. Inoue, M., Kuroumaru, M., Yoshida, S., Minami, T., Yamada, K., and Furukawa, M., Effect of Tip Clearance on Stall Evolution Process in a Low-Speed Axial Compressor Stage, ASME Turbo Expo 2004, GT2004-53354, 2004.06.
60. Yamada, K., Furukawa, M., Inoue, M., and Funazaki, K., Numerical Analysis of Tip Leakage Flow Field in a Transonic Axial Compressor Rotor, International Gas Turbine Congress 2003 Tokyo, TS-030, 2003.11.
61. Funazaki, K., Yamada, K., and Kato, Y., Studies on Effects of Periodic Wake Passing upon a Blade Leading Edge Separation Bubble: Transitional Behaviors of Separated Boundary Layer, International Gas Turbine Congress 2003 Tokyo, TS-069, 2003.11.
62. Funazaki, K., Yamada, K., and Kato, Y., Studies on Effects of Periodic Wake Passing upon a Blade Leading Edge Separation Bubble: Experimental Investigation Using a Simple Leading Edge Model, ASME Turbo Expo 2003, GT2003-38281, 2003.06.
63. Yamada, K., Furukawa, M., and Inoue, M., Numerical Analysis of Rotating Stall Inception in an Axial Compressor Rotor, the Fifth JSME-KSME Fluids Engineering Conference, pp.1597-1602, 2002.11.
64. Funazaki, K., Favaretto, C. F. F., Yamada, K., Kamata, M. and Tanuma, T., Numerical Simulation of the Flow Field in a Turbine Stage with Upstream Tangential Flow Injection from the Outer Casing (Effects of the Injection Angle)
, the Fifth JSME-KSME Fluids Engineering Conference, 2002.11.
65. Furukawa, M., Saiki, K., Yamada, K., and Inoue, M., Unsteady Flow Behavior Due to Breakdown of Tip Leakage Vortex in an Axial Compressor Rotor at Near-Stall Condition, ASME Turbo Expo 2000, ASME Paper, No. 2000-GT-0666, 2000.05.
66. 古川雅人,才木一寿,山田和豊,井上雅弘, 軸流圧縮機動翼の失速点近傍における翼端漏れ渦の崩壊に伴う異常流動現象, 日本機械学会論文集B編, 66巻644号,pp. 1029-1037, 2000.04.
67. Saiki, K., Furukawa, M., Yamada, K., and Inoue, M., Anomalous Flow Phenomena in an Axial Compressor Rotor at Near-Stall Condition, the 4th International Joint Symposium between Kyushu University and Chungnam National University, pp. 108-117, 1999.10.
68. Furukawa, M., Inoue, M., Saiki, K., Yamada, K., The Role of Tip Leakage Vortex Breakdown in Compressor Rotor Aerodynamics, Transactions of ASME, Journal of Turbomachinery, 121, 3, 469-480, Vol. 121, No. 3, pp. 469-480, 1999.07.
69. Inoue, M., Furukawa, M., Saiki, K., and Yamada, K., Physical Explanations of Tip Leakage Flow Fields in an Axial Compressor Rotor, ASME Turbo Expo '98, ASME Paper, No. 98-GT-091, 1998.06.

九大関連コンテンツ