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木村 雄吉, 柳川 聡寛, Kimura Takeyoshi, Yanagawa Toshihiro 福井工業大学研究紀要. 第一部 (36) 55-62, 2006-03-18

Many investigators have precisely carried out the measurements of drag forces on a sphere and a cylinder. However, it has been difficult to expound the theory of the drag forces, because of the …

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小沢 康美, 木村 雄吉 関西支部講演会講演論文集 2006.81 (0), _14-4_-, 2006

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木村 雄吉, 柳川 聡寛, Kimura Takeyoshi, Yanagawa Toshihiro 福井工業大学研究紀要. 第一部 (35) 71-78, 2005-03-18

Optimum Mach number of hypersonic itransports has been setimated, where the energy cost becomes the lowest. The flight time and energy to reach a destination are obtained in cases of several flight …

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木村 雄吉, 村越 大貴, Kimura Takeyoshi, Murakoshi Hiroki 福井工業大学研究紀要. 第一部 (33) 103-110, 2003-03-20

The basic performance of the airplanes is expressed by a wing loading W/S and a wing power P/S, in which W, P and S show the weight, power and wing area, respectively. These wing loading and the …

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木村 雄吉, 村越 大貴 北陸信越支部総会・講演会　講演論文集 2003.40 (0), 149-150, 2003

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木村 雄吉, 山田 和文 北陸信越支部総会・講演会　講演論文集 2003.40 (0), 151-152, 2003

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木村 雄吉, 山田 和文, Kimura Takeyoshi, Yamada Kazufumi 福井工業大学研究紀要. 第二部 (32) 131-138, 2002-03-20

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木村 雄吉, 井藤 創, 小川 和彦 可視化情報学会誌 19 (72), 19-24, 1999

Spark technique was applied to qualitative velocity profile visualization in hypersonic flows over compression and expansion corners. For comparison, Schlieren measurement and numerical simulation …

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蔦原 道久, 木村 雄吉, 小川 和彦, 上田 素直 日本機械学会論文集Ｂ編 65 (631), 934-939, 1999

The authors proposed the method of performance improvement by blowing moist air for a water jet ship. The authors investigated on the performance of the water jet ship by blowing air into the nozzle …

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蔦原 道久, 木村 雄吉, 小川 和彦, 細川 泰宏 日本機械学会論文集Ｂ編 64 (619), 670-676, 1998

The Lattice vortex method (LVM) by introducing virtual vortices has been proposed by the authors. This paper has focused on the treatment of viscous diffusion of vortices. From the result of …

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佐伯 祐志, 木村 雄吉, 小川 和彦 日本航空宇宙学会誌 46 (529), 93-99, 1998

To clarify the action of the rudder of HSTs, a hypersonic concave flow separation was studied. In hypersonic flows the rudder can not act efficiently because of the boundary layer separation, so …

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佐伯 祐志, 木村 雄吉, 小川 和彦 日本航空宇宙学会誌 46 (529), 100-110, 1998

To clarify the action of the rudder of HSTs, a hypersonic convex flow separation was studied. In a hypersonic flow the rudder can not act efficiently because of the boundary layer separation, so …

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木村 雄吉, 井藤 創, 小川 和彦 可視化情報学会誌 17 (Supplement2), 69-72, 1997

Spark technique was applied to qualitative velocity profile visualization in hypersonic flows over compression and expansion corners. For comparison, Schlieren measurement and numerical simulation …

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木村 雄吉, 小川 和彦 日本機械学会論文集Ｂ編 63 (606), 360-365, 1997

The purpose of this study is to clarify the effectiveness of sintered metal in cavitation erosion. For measurement of cavitation erosion, a decrease in the test time is desirable because present …

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木村 雄吉, 井藤 創, 小川 和彦 日本機械学会論文集Ｂ編 63 (610), 2017-2022, 1997

The afterglow technique was applied to visualize hypersonic flow past a compression corner and that past an expansion corner. The experiments were conducted at the Kobe University hypersonic shock …

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蔦原 道久, 木村 雄吉, 小川 和彦, 細川 泰宏 日本機械学会論文集Ｂ編 63 (614), 3209-3215, 1997

Lattice vortex method by introducing virtual vortices has been proposed in this paper. In our method, a staggered lattice for the velocity and the vorticity is used and the virtual vortices are …

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木村 雄吉, 小川 和彦, 井藤 創 日本機械学会論文集Ｂ編 63 (607), 932-937, 1997

A diaphragmless shock tunnel is developed using a butterfly valve, which has generally lower energy loss than that of a piston valve. The valve and its driving unit can be made from commercially …

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木村 雄吉, 井藤 創, 小川 和彦 日本航空宇宙学会誌 44 (512), 550-555, 1996

A shock tube theory is developed by considering the energy loss at the diaphragm section. By using the theory, a shock tube flow with a finite diaphragm opening time can be obtained. From the …

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木村 雄吉, 井藤 創, 小川 和彦 日本航空宇宙学会誌 44 (510), 423-428, 1996

The effects of angle of attack α on viscous hypersonic flowfield over a flat plate with a slightly blunt leading edge were examined theoretically and experimentally. An analytical solution which …

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虜 基徳, 王 忠益, 蔦原 道久, 木村 雄吉 日本機械学会論文集Ｂ編 62 (604), 4054-4059, 1996

A method for simulating flow of extremely low Reynolds number in a vortex-in-cell (VIC) was studied. The viscous diffusion was represented by the random walk method. The validity of this method was …

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木村 雄吉, 田中 隆治, 小川 和彦, 藤本 香代 日本舶用機関学会誌 30 (6), 448-452, 1995

There are several stages of Cavitation phenomena in the flow around butterfly valves. The cavitation stage such as cavitation inception, supercavitation inception, cavitation damage inception, …

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坂本 雅彦, 蔦原 道久, 木村 雄吉 日本機械学会論文集Ｂ編 61 (590), 3728-3734, 1995

We describe here an experimental study of a new type of nozzle which generates a high-speed two-phase water jet as a propulsion device for aship. In order to investigate performance improvement of …

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蔦原 道久, 坂本 雅彦, 木村 雄吉 日本機械学会論文集Ｂ編 61 (583), 1029-1034, 1995

In this paper we describe an experimental study of a new type of nozzle which generates a high-speed two-phase water jet as a propulsion device for a ship. In order to investigate the performance …

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Ro, D.S., 木村, 雄吉, 小川, 和彦, Ro, Dae Sung, Kimura, Takeyoshi, Ogawa, Kazuhiko 航空宇宙技術研究所特別資料: 第11回航空機計算空気力学シンポジウム論文集 = Special Publication of National Aerospace Laboratory: Proceedings of the 11th NAL Symposium on aircraft computational aerodynamics 22 73-78, 1994-03

航空宇宙技術研究所 10-11 Jun. 1993 東京 日本

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蔦原 道久, 王 忠益, 木村 雄吉 日本航空宇宙学会誌 42 (481), 116-124, 1994

Two dimensional viscous flows past a rotating circular cylinder are numerically calculated by the Vortex-in-Cell (VIC) method. The Random Walk method is used to simulate the diffusion of the …

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蔦原 道久, 坂本 雅彦, 木村 雄吉, 橋本 潔 日本機械学会論文集Ｂ編 60 (578), 3372-3378, 1994

The purpose of this study is to investigate a new type of nozzle which generates a high-speed two-phase water jet as a propulsion device for a ship. In order to examine the characteristics of the …

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蔦原 道久, 木村 雄吉 日本機械学会論文集Ｂ編 60 (571), 910-915, 1994

A fan using the Weis-Fogh mechanism was built and its characteristics were studied. Two wings were set to move out-of-phase by an arm which rotates changing its directions in a square channel. …

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木村 雄吉, 小川 和彦, 上原 到, 桑田 千照 日本舶用機関学会誌 28 (11), 709-716, 1993

The purposes of this sutdy are to clarify the characteristics of cavitation erosion in piping line behind a butterfly valve and to propose the method of predicting the erosion resistance.<BR>One of …

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蔦原 道久, 冨山 明男, 木村 雄吉, 村田 浩 日本機械学会論文集Ｂ編 59 (564), 2477-2483, 1993

Cellular automata have been used recently for simulations of fluid motion. However, applications of this method have been limited to flows with unchanged cinfigurations becase of difficulty with the …

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蔦原 道久, 坂本 雅彦, 木村 雄吉, 橋本 潔, 美濃 雅彦 日本機械学会論文集Ｂ編 59 (565), 2868-2874, 1993

This paper proposes a new type of nozzle which generates a high-speed two-phase water jet as a propulsion device for a ship. The high-pressure gas accelerates the two-phase jet by temporal and local …

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高橋 邦雄, 蔦原 道久, 木村 雄吉 日本機械学会論文集Ｂ編 58 (552), 2425-2430, 1992

A numerical analysis is performed for a rotary pump using the Weis-Fogh mechanism, which is a lift-generation mechanism in the hovering flight of small insects. Two-dimensional flow past a rotor in …

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蔦原 道久, 木村 雄吉, 高橋 邦雄 日本機械学会論文集Ｂ編 58 (553), 2793-2798, 1992

Effects of control of the wings and the adjustment of the channel shape were studied experimentally, concerning the performance of a rotary pump using the Weis-Fogh mechanism. The opening angle was …

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木村 雄吉, 蔦原 道久, 王 忠益, 石井 裕 可視化情報学会誌 11 (Supplement1), 107-110, 1991

Flows past a rotating circular cylinder was investigated by using the dye injection method, and a computer simulation using the Vortex-in-Cell method was carried out. Results obtained by the two …

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蔦原 道久, 木村 雄吉, 高橋 邦雄 可視化情報学会誌 11 (Supplement1), 103-106, 1991

A pump of rotary type using the Weis-Fogh mechanism, which is a mechanism of lift generation in the hovering flight of small insects, was studied numerically using the discrete vortex method. A …

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蔦原 道久, 木村 雄吉, 高橋 邦雄 日本機械学会論文集Ｂ編 57 (535), 983-987, 1991

Characteristics of the pump in a square channel using the Weis-Fogh mechanism, which is the lift generation mechanism in the hovering flight of small insects, are studied in this paper. The wing …

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蔦原 道久, 木村 雄吉, 高橋 邦雄 日本機械学会論文集Ｂ編 57 (542), 3439-3443, 1991

A pilot pump of the rotary type using the Weis-Fogh mechanism, which is a lift generation mechanism in the hovering flight of small insects, was built, and its characteristics were studied …

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蔦原 道久, 木村 雄吉, 橋本 潔 日本機械学会論文集Ｂ編 57 (535), 977-982, 1991

A new type of nozzle generating a two-phase high-speed water jet is presented. The structure is of simple convergent and divergent type. High pressure air is injected into the water flow through …

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蔦原 道久, 木村 雄吉, 盧 基徳, 高橋 邦雄 日本機械学会論文集Ｂ編 56 (525), 1299-1305, 1990

The effects of side walls of a channel in which a two-dimensional model of the Weis-Fogh mechanism is equipped are experimentally investigated. The effects of the elasticity of the spring which …

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盧 基徳, 蔦原 道久, 木村 雄吉 日本機械学会論文集Ｂ編 56 (525), 1290-1298, 1990

The flowfield of a ship's propulsion mechanism consisting of two-series of wings in a square channel is visualized by numerical simulations using the discrete vortex method and by the hydrogen …

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西尾 正富, 木村 雄吉 日本機械学会論文集Ｂ編 56 (532), 3799-3804, 1990

This paper describes a new method of measuring fluid pressure by means of a magnetic tape. First, a pressure transducer using a magnetic tape was made for trial, and pressure measurements around a …

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木村 雄吉, 蔦原 道久, 鎌田 憲二, 生島 嘉大 可視化情報学会誌 10 (1Supplement), 73-78, 1990

It is shown that a groove whose shape is circular-arc has an effect on moving the separation point backward. Flow visualizations are performed by the hydrogen bubble method and the dye injection …

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木村 雄吉, 蔦原 道久, 王 忠益, 石井 裕 流れの可視化 9 (34), 273-276, 1989

Flows past a circular cylinder is a classical problem of the fluid mechanics and it is well known that the Karman vortices disappear when the rotating speed is large. But the dependence of this …

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西尾 正富, 木村 雄吉 流れの可視化 9 (34), 349-354, 1989

This paper described a new visualizing method of streamlines around a body in hypersonic flows. The visualization of a streamline around a wedge was tried and the visualized result was compared with …

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盧 基徳, 蔦原 道久, 木村 雄吉 流れの可視化 8 (30), 205-208, 1988

The flowfield of a ship's propulsion mechanism consisting of two-series wings in a square channel are visualized by numerical simulations using a personal computer and by the hydrogen-bubble …

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蔦原 道久, 木村 雄吉, 盧 基徳 日本舶用機関学会誌 23 (8), 474-479, 1988

A two-dimensional model of the Weis-Fogh mechanism, which is a mechanism of hovering flight of small insects, is applied to ship propulsion. A model of the propulsion mechanism consisting of one or …

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蔦原 道久, 木村 雄吉 日本機械学会論文集Ｂ編 54 (498), 393-397, 1988

An application of the Weis-Fogh mechanism to pumps was studied. A pilot pump was built and the characteristics were investigated experimentally, and it was shown that this mechanism works well for …

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蔦原 道久, 木村 雄吉, 盧 基徳 日本航空宇宙学会誌 36 (417), 473-479, 1988

This paper presents a method for calculation of the unsteady force, the moment, and the pressure distribution on the body in a two dimensional flow using the discrete vortex method. The body surface …

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木村 雄吉 日本機械学会誌 91 (837), 775-, 1988

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蔦原 道久, 木村 雄吉, 廬 基徳 日本機械学会論文集Ｂ編 54 (507), 3165-3170, 1988

The dynamic properties of a ship's propulsion mechanism consisting of two-series wings in a square channel are experimentally investigated. The time history of the trust and the drag acting on the …

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蔦原 道久, 木村 雄吉 日本機械学会論文集Ｂ編 54 (501), 1088-1094, 1988

The dynamic properties of a ship's propulsion mechanism using the Weis-Fogh mechanism are studied by the discrete vortex method. The wing in the channel is approximated by a finite number of bound …

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蔦原 道久, 木村 雄吉, 盧 基徳 日本機械学会論文集Ｂ編 53 (496), 3711-3715, 1987

A model of a ship's propulsion mechanism is proposed, in which two-series flat wings are arranged in a square channel. The motion of each wing is the same as that of the single-stage model …

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蔦原 道久, 木村 雄吉 日本航空宇宙学会誌 35 (407), 596-604, 1987

Aerodynamic characteristics of the Weis-Fogh mechanism which is a lift generating mechanism of hovering flight of small insects were studied by the discrete vortex method. Two flat wings were …

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蔦原 道久, 木村 雄吉 流れの可視化 6 (22), 301-306, 1986

Flow patterns in a two-dimensional model of the Weis-Fogh mechanism are investigated by the discrete vortex method and a flow-visualization technique using tracers of aluminum particles. Two cases …

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木村 雄吉, 小川 和彦 日本機械学会論文集Ｂ編 52 (474), 501-507, 1986

ちょう形弁に発生するキャビテーションの振動および騒音の特定な周波数帯に着目し,その周波数帯の振動および騒音の測定を行い,キャビテーション状態の評価を与えた.初生は特定周波数帯の振動が急激に大きくなることから判定できる.成長状態は特定周波数帯の騒音が急上昇することから判定することが可能である.撮影結果と測定結果を検討し,ちょう形弁に発生するキャビテーションの実用的な観点からの証価が可能であることを…

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木村 雄吉, 蔦原 道久 日本航空宇宙学会誌 34 (387), 188-194, 1986

Flows past a rotating circular cylinder at high Reynolds number are investigated by a discrete vortex method. The nascent vortices are introduced to the flowfield at each time step from several …

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蔦原 遺久, 木村 雄吉 日本機械学会論文集Ｂ編 52 (477), 2143-2147, 1986

The properties of the model of a ship's propulsion mechanism using the so-called Weis-Fogh mechanism are investigated. The above model, proposed in the previous paper by the same authors, consists …

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山里, 栄昭, 伊良部, 邦夫, 木村, 雄吉, Yamazato, Eisho, Irabu, Kunio, Kimura, Takeyoshi 琉球大学工学部紀要 (29) 1-20, 1985-03

Experimental study of the two-dimensional diffusers with wake-type inlet velocity profiles in the parallel walls was carried out. The purpose of this study is to investigate the effects of …

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木村 雄吉, 小川 和彦 流れの可視化 5 (Supplement), 15-18, 1985

When cavitation around a butterfly valve becomes very intense, cavitation bubbles flow downstream without collapses. As the flow velocity is increased further, a cave whose shape is like a wedge is …

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橋本 啓介, 木村 雄吉 日本機械学会論文集Ｂ編 51 (464), 1216-1224, 1985

高亜音速領域での高負荷特性に加え,低損失の広範な作動特性,入射角特性を目標として境界層状態の最適化がなされた 翼面速度分布を入力条件として改良形流路解法逆問題設計手法を用いた翼形開発が行われた.高速二次元翼列試験結果,設計法の有効性や,一定の空力性能水準にあるaft-loaded通常翼形に比べ優れた翼列特性を確認した.これらの翼列は,軸流ガスタービン段重畳,翼枚数の低減化,部分負荷性能向上を達成…

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蔦原 道久, 木村 雄吉 日本機械学会論文集Ｂ編 51 (470), 3137-3144, 1985

小ばちの静止飛行の観察から新しく発見された,Weis-Fogh(ヴァイスファー)メカニズムと呼ばれる,効率のよい揚力発生のメカニズムを,船舶の推進に応用するため,二次元の推進機構のモデルを提案した。そして,その一行程における翼の開く過程,並進運動の過程,閉じる過程のそれぞれに対し,ポテンシャル流れの仮定で等角写像を用いて解析を行い,その力学的特性を明らかにするとともに,この推進機構の有効性を予測…

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蔦原 道久, 木村 雄吉 日本航空宇宙学会誌 33 (379), 458-460, 1985

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蔦原 道久, 木村 雄吉 日本航空宇宙学会誌 32 (362), 154-162, 1984

LIGHTHILL's two-dimensional inviscid-fiow model (1973) for the WEIS-FOGH mechanism is investigated. For the 'fling' (or opening) stage, the lift and the moment acting on the wing are calculated from …

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木村 雄吉, 西尾 正富 流れの可視化 4 (15), 425-429, 1984

This paper is concerned with the shock wave visualization using an electric discharge. In the previous discharge method, point-point electrodes had been used to generate electric discharges. The …

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木村 雄吉, 西尾 正富, 小竹 睦夫 日本航空宇宙学会誌 32 (368), 511-517, 1984

The steady hypersonic flow around a slender conical flat-top wing-body has been solved by applying the equivalence principle, which is the theory that the problem of steady hypersonic flow past a …

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木村 雄吉, 西尾 正富 流れの可視化 2 (7), 661-666, 1982

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斉藤 浩, 木村 雄吉, 坂本 知紀 栄養と食糧 29 (7), 404-408, 1976

For the purpose of finding antioxidative spices, periodical POV changes of lard containing each of 27 different types of ground spices were quantitatively determined by the modified Lea method and …

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斉藤 浩, 木村 雄吉, 坂本 知紀 栄養と食糧 29 (9), 505-510, 1976

The antioxidant effects of petrolium ether soluble fractions from ground spices on lard were studied and compared with those of BHA and tocopherols.<BR>The results obtained are summerized as …

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神元 五郎, 木村 雄吉, 西田 迪雄, 堀内 立 日本航空学会誌 16 (170), 67-74, 1968

In argon and nitrogen plasma jet flows, the electron density measurements were made with microwave interferometer. <BR>The obtained electron number density in the center of the flow was in the range …

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神元 五郎, 木村 雄吉, 松為 宏幸, 上中 義敞, 塚本 明正 日本航空学会誌 16 (179), 418-424, 1968

The many informations about the performances of the gun tunnel had been obtained theoretically and experimentally by the pilot gun tunnel which was constructed at Kyoto University in 1962. By these …

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神元 五郎, 木村 雄吉, 手島 光司 日本航空学会誌 15 (158), 71-78, 1967

Motion of a heavy piston which makes isentropic compression has been studied. Theoretical piston motions are calculated and presented. Experimental data of stagnation pressure and duration time with …

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木村 雄吉 日本航空学会誌 15 (165), 329-334, 1967

In a hypersonic flow, an analysis of the flow around a spherically blunted cone was carried out by applying the equivalence principle. The present experiments were carried out at Mach numbers of 10 …

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神元 五郎, 木村 雄吉, 上中 義敞, 橋本 晃, 橋本 宏行 日本航空学会誌 15 (166), 373-380, 1967

The hypersonic aerodynamic chracteristics of spherically blunted half cones were measured in the Kyoto University pilot gun-tunnel at Mach number 10, Reynolds Number 0. 42×10<SUP>5</SUP>/cm and …

DOI Web Site

神元 五郎, 手島 光司, 木村 雄吉 日本航空学会誌 13 (143), 388-395, 1965

DOI Web Site

神元 五郎, 森 敏一, 木村 雄吉, 河内 国昭 日本航空学会誌 12 (131), 418-423, 1964

A microwave interferometer for determining piston motions in a hypersonic gun tunnel was developed. Owing to the specially designed microwave feeder, measurements of the piston motion with good …

DOI Web Site 被引用文献1件

神元 五郎, 森 敏一, 木村 雄吉 日本航空学会誌 12 (131), 411-417, 1964

A theoretical analysis and some experimental results of the piston motion in the hypersonic gun tunnel are contained in this paper. The piston motion has close effects upon the uniformity of flow at …

DOI Web Site 被引用文献1件

神元 五郎, 森 敏一, 木村 雄吉 日本航空学会誌 11 (117), 306-310, 1963

This report is described of the mode of the operation and the characteristics of the hypersonic gun tunnel built at Kyoto University. The theoretical calcutations are presented of the piston motion, …

DOI Web Site 被引用文献1件

木村 雄吉 科学基礎論研究 4 (1), 6-7, 1958

DOI

木村,雄吉, 丹羽,孝 動物学雑誌 65 (3・4), 125-, 1956-04-15

NDLデジタルコレクション 医中誌

木村,雄吉, 伊藤,薫, 藤井,隆 動物学雑誌 63 (3・4), 134-, 1954-04-15

NDLデジタルコレクション

木村,雄吉, 丹羽,孝, 藤井,隆, 石田,壽老 動物学雑誌 63 (3・4), 134-135, 1954-04-15

NDLデジタルコレクション

中 脩三, 岡本 彰祐, 高垣 玄吉郎, 山本 達也, 木村 雄吉 生体の科学 5 (4), 188-190, 1954-02-15

DOI

木村,雄吉, 丹羽,孝, 藤井,隆 動物学雑誌 62 (3・4), 144-, 1953-04-15

NDLデジタルコレクション 医中誌

木村 雄吉 動物学雑誌 48 (8-10), 603-615, 1936-10-15

A set of apparata for hydrogenation, filtration and evaporation was designed and constructed for this purpose. Conditions of hydrogenation were found to be as follows: solvent: ethyl alcohol; …

DOI NDLデジタルコレクション

木村,雄吉 動物学雑誌 48 (8-10), 433-435, 1936-10-15

NDLデジタルコレクション