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Shinichiro Ogawa
Shinichiro Ogawa
Osaka Metropolitan University, Department of Aerospace Engineering, Assistant professor
在 omu.ac.jp 的电子邮件经过验证
标题
引用次数
引用次数
年份
Application of immersed boundary method with wall injection for solid rocket motor internal flow
T Hirose, S Ogawa, D Sasaki, Y Fukushima, S Obayashi
AIAA Modeling and Simulation Technologies Conference, 1944, 2017
62017
An Experimental Investigation on Forced Ignition Characteristics of Hydrocarbon Mixture Fuel in Scramjet Combustor
S Ogawa, K Kobayashi, S Tomioka
Asia-Pacific International Symposium on Aerospace Technology, 1381-1395, 2021
52021
Two-dimensional computational fluid dynamics analysis of internal flow in a simplified solid rocket motor combustion chamber
S Ogawa, D Sasaki
Journal of Fluid Science and Technology 12 (3), JFST0023-JFST0023, 2017
52017
Forced ignition modeling of methane-ethylene mixtures in scramjet combustors
S Ogawa, K Kobayashi, S Tomioka
Combustion and Flame 263, 113383, 2024
32024
Study on the Ignition Method for n-Octane Pyrolysis Fuel in a Scramjet Engine
S Ogawa, K Kobayashi, S Tomioka
Transactions of the Japan Society for Aeronautical and Space Sciences 65 (1 …, 2022
32022
Evaluation of Exhaust Gas from Micro-Jet Engine using SAF Made from Coconut
S Ogawa, T Hongo, K Mori, Y Maeda, NH Uyen
AIAA SCITECH 2024 Forum, 0105, 2024
12024
Three-Dimensional Fluid Analysis for Internal Flow of a Solid Rocket Motor with Nozzle Using Building-Cube Method
S Ogawa, K Ouchi, D Sasaki
Aerospace Technology Japan 22, 1-10, 2023
12023
Development of Wall Injection Model for Solid Rocket Motor Internal Flow by Block-Structure Cartesian Mesh
S Ogawa, D Sasaki
AIAA SCITECH 2023 Forum, 1131, 2023
12023
Dynamic Mode Decomposition of the Combustion Flow Field in a Scramjet Combustor with a Cavity Flameholder
S Ogawa
AIAA AVIATION 2023 Forum, 3787, 2023
12023
Study on Ignition of Thermally Cracked Hydrocarbon Fuel in Scramjet Combustors
S OGAWA
Tohoku University, 2021
12021
Influence on ignition characteristic by the difference of methane/ethylene mixture gas rate
S Ogawa, K Nojima, K Kobayashi, S Tomioka
2018 Joint Propulsion Conference, 4777, 2018
12018
Mechanisms of ignition and combustion instability in a scramjet combustor with micro-rocket torch using dynamic mode decomposition
S Ogawa
Physics of Fluids 36 (10), 2024
2024
Development of a Radial Injection Flow Model of a Cylinder Simulating a Solid Rocket Motor Geometry using the Building-Cube Method
S OGAWA, D SASAKI
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 67 (6 …, 2024
2024
Study on Combustion Characteristics of Coconut SAF Using Micro Jet Engine
S Ogawa, K Mori, Y Maeda
International Journal of Gas Turbine, Propulsion and Power Systems 15 (5 …, 2024
2024
Modal Analysis of Forced Ignition Characteristics using Micro-Rocket Torch in Supersonic Flow
S OGAWA
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 67 (2 …, 2024
2024
Effect of Burning Surface Regression on Internal Flow Field in Solid Rocket Motor
S Ogawa, D Sasaki, S Yoshinaga
AIAA SCITECH 2024 Forum, 0213, 2024
2024
Development of combustion gas measurement systems for micro-rocket torch using a diode laser sensor
Y HIRAYAMA, S OGAWA
Mechanical Engineering Letters 9, 23-00261-23-00261, 2023
2023
直交格子積み上げ法によるノズル付き固体燃料ロケット内部流れの 3 次元流体解析
小川秦一郎, 大内健太郎, 佐々木大輔
航空宇宙技術 22, 1-10, 2023
2023
Study on ignition of thermally cracked hydrocarbon fuel in scramjet combustors
小川秦一郎
Tohoku University, 2021
2021
Influence of Temperature and Mixture Gas Ratio to Autoignition of n-Octane Pyrolysis Gas
S Ogawa, T Miyaura, K Kobayashi, S Tomioka
AIAA Propulsion and Energy 2019 Forum, 4126, 2019
2019
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