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H
Harunori Nagata
hokkaido university
19
H指数
326
论文数
1.2K
被引数
0
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14
发表时间
发表时间
IF
被引数
Experimental elucidation of the combustion-mode transition in a liquid oxygen-solid fuel duct
液氧-固体燃料管道中燃烧模式转换的实验阐释
Proceedings of the Combustion Institute
IF
5.2
2026-07-01
0
PRE
AI
Yamaguchi, Mao; Suzuki, Sho; Son, Taejun; Takahashi, Shunya; Kumagai, Moeka; Nagata, Harunori
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Physical mechanism of regression to flame spread transition under opposed forced flows in internal fuel pipes applied to AIEB rocket
内部燃料管中逆向强制流作用下从回退到火焰蔓延转变的物理机制及其在AIEB火箭中的应用
Fuel
IF
7.5
2025-08-12
0
PRE
AI
Giuseppe Gallo; Mai Fukada; Harunori Nagata
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Regenerative cooling in hybrid rocket engines based on Self-Pressurized liquid nitrous oxide
APPLIED THERMAL ENGINEERING
IF
6.9
2024-10-01
1
PRE
AI
Gallo, Giuseppe; Miyahara, Yuta; Kamps, Landon; Nagata, Harunori
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Phenomenological regression rate model in axial injection end-burning hybrid rocket motor using different oxidizers
使用不同氧化剂的轴向喷射端燃混合火箭发动机的现象学回归速率模型
COMBUSTION AND FLAME
IF
6.2
2024-05-01
0
PRE
AI
Gallo, Giuseppe; Fukada, Mai; Suzuki, Sho; Nagata, Harunori
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Experimental investigation of regenerative cooling performance in hybrid rocket engines
THERMAL SCIENCE AND ENGINEERING PROGRESS
IF
5.4
2024-03-01
5
PRE
AI
Gallo, Giuseppe; Kojima, Hiroki; Kamps, Landon; Nagata, Harunori
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Prediction of the fuel regression-rate in a HDPE single port hybrid rocket fed by liquid nitrous oxide
COMBUSTION AND FLAME
IF
6.2
2024-01-01
6
PRE
AI
Gallo, Giuseppe; Kamps, Landon; Hirai, Shota; Carmicino, Carmine; Harunori, Nagata
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One-dimensional modelling of the nozzle cooling with cryogenic oxygen flowing through helical channels in a hybrid rocket
ACTA ASTRONAUTICA
IF
3.4
2023-09-01
7
PRE
AI
Gallo, Giuseppe; Kamps, Landon; Hirai, Shota; Carmicino, Carmine; Nagata, Harunori
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Controlling heat release of crystallization from supercooling state of a solid-solid PCM, 2-amino-2-methyl-1,3-propanediol
控制固体-固体PCM,2-氨基-2-甲基-1,3-丙二醇的过冷状态的结晶放热
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER
IF
5.8
2019-07-01
10
PRE
AI
Gotoh, Ryohei; Totani, Tsuyoshi; Wakita, Masashi; Nagata, Harunori
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Transition characteristics of combustion modes for flame spread in solid fuel tube
COMBUSTION AND FLAME
IF
6.2
2012-07-01
15
PRE
AI
Matsuoka, Tsuneyoshi; Murakami, Shota; Nagata, Harunori
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Combustion characteristics of the end burning hybrid rockets in laminar flow
ACTA ASTRONAUTICA
IF
3.4
2011-01-01
5
PRE
AI
Matsuoka, Tsuneyoshi; Nagata, Harunori
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Determining factor for the blowoff limit of a flame spreading in an opposed turbulent flow, in a narrow solid-fuel duct
COMBUSTION AND FLAME
IF
6.2
2006-11-01
26
PRE
AI
Hashimoto, Nozomu; Nagata, Harunori; Totani, Tsuyoshi; Kudo, Isao
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Development of CAMUI hybrid rocket to create a market for small rocket experiments
ACTA ASTRONAUTICA
IF
3.4
2006-07-01
42
OA
AI
Nagata, Harunori; Ito, Mitsunori; Maeda, Takenori; Watanabe, Mikio; Uematsu, Tsutomu; Totani, Tsuyoshi; Kudo, Isao
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Numerical and experimental studies on circulation of working fluid in liquid droplet radiator
ACTA ASTRONAUTICA
IF
3.4
2006-07-01
13
OA
AI
Totani, T; Kodama, T; Watanabe, K; Nanbu, K; Nagata, H; Kudo, I
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Interactive combustion of two-dimensionally arranged quasi-droplet clusters under microgravity
COMBUSTION AND FLAME
IF
6.2
2002-06-01
13
OA
AI
Nagata, H; Kudo, I; Ito, K; Nakamura, S; Takeshita, Y
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研究方向
暂时未获取到该数据
合作学者
合作期刊
K
Kenichi Ito
H 指数: 44 · 论文数: 394
I
Isao Kudo
H 指数: 29 · 论文数: 255
N
Nozomu Hashimoto
H 指数: 29 · 论文数: 158
T
Takuya Kodama
H 指数: 23 · 论文数: 207
K
Kensuke Watanabe
H 指数: 22 · 论文数: 215
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