出版者・発行元：Energy  

To uncover the microscopic reaction mechanisms of dimethyl ether (DME) pyrolysis and oxidation, reactive molecular dynamics simulations were employed to investigate the reaction processes under various O2/DME ratios and impurity environments at 2200 K–3200 K. The results show that DME pyrolysis begins with a decomposition reaction of CH3OCH3 → CH3O + CH3, ultimately leading to the formation of CO, H2 and PAHs. The reaction pathways of DME oxidation contain light gas conversion and combustion. In fuel rich conditions, the oxidation produces mainly H2 and CO, while in fuel lean conditions, the oxidation products tend to be H2O and CO2. The carbon components of DME are completely converted into CO2 and CO regardless of O2 content. In the presence of impurities H2O or CO2, the oxidation reaction pathway is altered, causing consumption and transformation of these impurities into active radicals such as OH, further promoting the progress of the reaction. The top three light gases produced are hydrogen, methanol and methane, and increasing H2 production in the DME oxidation process can be achieved through both oxygen subtraction and water addition. The rate of formaldehyde generation during pyrolysis is higher than that during oxidation. However, a higher oxygen content leads to increased formaldehyde production.

DOI： 10.1016/j.energy.2024.131013

Web of Science

Scopus

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1299/jtst.24-00087

出版者・発行元：Energy and Fuels  

The combustion characteristics of cracked NH3 flames are investigated experimentally and numerically. The one-dimensional (1D) calculations are performed to validate the accuracy of the reaction mechanisms in cracking conditions and to understand the fundamental characteristics of the cracked NH3 flames. In the experiments, the local distributions of OH and NO and the species emissions of NO, NO2, N2O, and NH3 are measured using hydroxyl radical planar laser-induced fluorescence (OH-PLIF), NO* chemiluminescence, and Fourier transform infrared (FTIR) spectroscopy, respectively. The effects of partial cracking on the flame structure and emission characteristics are investigated. In addition, the large eddy simulations (LESs) with flamelet-generated manifold (FGM) methods, which consider the preferential diffusion effect, are conducted to understand the validity of the LES and to further elucidate the effects of the cracking ratio (Cr) on cracked NH3 flames. The 1D calculation results show that reaction mechanisms by Mei et al. ( Mei, B. ; Zhang, J. ; Shi, X. ; Xi, Z. ; Li, Y. Enhancement of ammonia combustion with partial fuel cracking strategy: Laminar flame propagation and kinetic modeling investigation of NH3/H2/N2/air mixtures up to 10 atm. Combust. Flame 2021, 231, 111472, 10.1016/j.combustflame.2021.111472), Shrestha et al. ( Shrestha, K. P. ; Lhuillier, C. ; Barbosa, A. A. ; Brequigny, P. ; Contino, F. ; Mounaïm-Rousselle, C. ; Seidel, L. ; Mauss, F. An experimental and modeling study of ammonia with enriched oxygen content and ammonia/hydrogen laminar flame speed at elevated pressure and temperature. Proc. Combust. Inst. 2021, 38, 2163−2174, 10.1016/j.proci.2020.06.197), and Otomo et al. ( Otomo, J. ; Koshi, M. ; Mitsumori, T. ; Iwasaki, H. ; Yamada, K. Chemical kinetic modeling of ammonia oxidation with improved reaction mechanism for ammonia/air and ammonia/hydrogen/air combustion. Int. J. Hydrogen Energy 2018, 43, 3004−3014, 10.1016/j.ijhydene.2017.12.066) have acceptable accuracies for predicting combustion characteristics of cracked NH3 flames. As the cracking ratio increases, the ignition delay time (tig) and laminar flame speed (Sl) are shortened and accelerated, respectively, and the effect of Cr on Sl becomes evident in higher ϕ conditions. The NO emissions exhibit a tendency to achieve peaks around Cr = 0.6-0.9, irrespective of ϕ. The experimental results show that the partial cracking significantly changes the NH3 swirl flame structure. As Cr increases, the flames changed from “V” to “M” shape and the OH and NO* signals are enhanced. While OH and NO* signals show a strong positive correlation in a pure NH3 flame, the correlation gradually weakens when Cr increases. As Cr increases, the NO and NO2 emissions increase, whereas the NH3 emissions decrease. As a result, the optimal condition for minimizing global emissions is considered to be Cr = 0.2. By comparison of the velocity and OH fields to the experiments, it is verified that the present LESs coupled with the FGM combustion model, considering the preferential diffusion effect, capture the general feature of the cracked NH3 swirl flames well. The heat release rate (HRR) is enhanced as a result of partial cracking. A higher Cr enables the flame to stabilize even in highly strained areas of the flame front. As Cr increases, the amount of both fuel NO and thermal NO increases as a result of higher O and OH and higher temperature. However, these are reduced by increasing ϕ and enhancing heat loss through walls.

DOI： 10.1021/acs.energyfuels.4c00312

Scopus

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1021/acs.energyfuels.4c00312

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1299/mej.23-00400

出版者・発行元：Journal of Computational Physics  

A new semi-implicit pressure-based solver considering the real gas effect is developed and tested. The advantage of the semi-implicit solver is that it can take a large time step, which makes the calculation speed faster than the classical density-based explicit solver. The comparison of the calculation speed between the explicit density-based solver and the new semi-implicit pressure-based solver is conducted by performing two-dimensional numerical simulations of a cryogenic nitrogen planar jet. Moreover, the developed pressure-based solver is validated by comparing the numerical results of a three-dimensional large-eddy simulation of a cryogenic nitrogen jet under the supercritical pressure condition with the experimental result. Results show that the developed pressure-based solver can calculate more than five times faster than the classical explicit density-based solver and accurately predict the jet behavior under the supercritical pressure condition.

DOI： 10.1016/j.jcp.2024.112782

Scopus

記述言語：英語   掲載種別：研究論文（学術雑誌）  

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.energy.2024.131013

出版者・発行元：Applications in Energy and Combustion Science  

Importance of the considerations of preferential diffusion and flame stretch effects in the flamelet-generated manifold (FGM) method on the prediction accuracy is investigated by two-dimensional numerical simulations of cylindrical NH3/air premixed flames, under the conditions of an unburnt gas temperature of 673 K, an ambient pressure of 2 MPa, and equivalence ratios of 0.8 to 1.2. Results of the numerical simulations using the detailed chemistry, in which 32 species and 204 reactions are directly solved in the physical space without the FGM method, show that the mixture fraction in the burnt gas increases from the unburnt gas value when considering the preferential diffusion effect, whereas it remains flat when assuming the unity Lewis number. This means that assuming the unity Lewis number causes the underprediction and overprediction of the burnt gas temperature under fuel-lean and fuel-rich conditions, respectively. Results of the numerical simulations using the FGM methods show that considering the preferential diffusion and flame stretch effects in the FGM method is important for accurate prediction of the flame propagating speed, and the effectiveness is more evident for the flame stretch effect than for the preferential diffusion effect for the NH3/air premixed flames.

DOI： 10.1016/j.jaecs.2024.100253

Web of Science

Scopus

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.jaecs.2024.100253

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.jcp.2024.112782

出版者・発行元：International Journal of Gas Turbine, Propulsion and Power Systems  

To design a low-emission hydrogen-fired gas turbine combustor, prevention of flashback is one of key issues. However, the detailed measurement of flashback is difficult and expensive, especially at the actual operation condition. Therefore, the high-precision numerical simulation technology is important to study the mechanism and countermeasures of flashback. In this study, a large eddy simulation (LES) using a non-adiabatic flamelet-generated manifold (NA-FGM) approach, considering the effects of heat loss, is applied to simulate hydrogen-air premixed flame propagating in a rectangular channel. Then, the validity of predicting flashback limits is examined. The results show that the NA-FGM approach quantitatively well captures the flashback limits variation observed in the experiments. This indicates that accounting for the influence of heat loss is crucial in achieving precise prediction of the flashback in developing a low-emission hydrogen gas turbine combustor.

DOI： 10.38036/jgpp.15.1_40

Scopus

出版者・発行元：Journal of Thermal Science and Technology  

One-dimensional numerical simulations of an unstretched propagating hydrogen/air premixed flame and two-dimensional numerical simulations of outwardly propagating hydrogen/air laminar premixed flames are performed using a flamelet-generated manifold (FGM) method. The effects of considering preferential diffusion and flame stretch in the FGM method are investigated in detail. The results of the one-dimensional numerical simulations show that the flame behavior can be qualitatively reproduced without considering both these two phenomena, but it can be predicted more precisely by considering preferential diffusion. On the other hand, the results of the two-dimensional numerical simulations show that considering both these two phenomena is essential to accurately predict the behavior of stretched hydrogen/air premixed flames at an equivalence ratio of less or more than 0.7. The results also show that the consideration of preferential diffusion and flame stretch is less important at an equivalence ratio of around 0.7. In addition, the validity of an assumption that the Lewis numbers of each species are constant, which is used in most previous studies, is investigated. The results show that assuming constant Lewis numbers worsens the prediction accuracy. The computational cost of the FGM method considering both preferential diffusion and flame stretch is about 1/15 that of the detailed calculation for the two-dimensional numerical simulations, which indicates the efficiency of the extended FGM method.

DOI： 10.1299/jtst.24-00087

Scopus

記述言語：英語   出版者・発行元：一般社団法人 日本機械学会  

DOI： 10.1299/mej.23-00400

Web of Science

CiNii Research

出版者・発行元：Proceedings of the Combustion Institute  

Direct numerical simulation with a detailed chemical reaction mechanism is performed for detonation-turbulence interaction in a stoichiometric hydrogen/oxygen mixture. Three turbulences are introduced into detonation with different intensities which are defined by turbulent Reynolds number and turbulent Mach number. The results show that turbulent flow corrugates both shock and flame fronts and makes cellular structures obscure and randomized. The strongest turbulence distorts the shock so strongly that the transverse wave is unclear and cellular structure is destroyed. Time-averaged one-dimensional profiles demonstrate that turbulence promotes the reaction progress. Stronger turbulence produces more intermediate species, by which the chemical reaction reaches completion more rapidly. The turbulent combustion regime indicates that small eddies intrude the flame structure, for which unburned gas pockets are broken into pieces and consumed rapidly. It is consistent with the tendency of the probability density function of induction length, which has only one peak in a smaller value under stronger turbulences, whereas two peaks under the weakest turbulence and without turbulence. Turbulence increases the peak pressure on one-dimensionally averaged structure except for the case where the cellular structure is destroyed. Averaged detonation velocity is strongly correlated with the magnitude of peak pressure, which is the lowest in the strongest turbulence, whereas its deviation increases with turbulent intensities. The absence of the cellular structure, which has been confirmed in optical measurements of rotating detonation engines, could be attributed to the collapse of the cellular structure observed in the strongest turbulence.

DOI： 10.1016/j.proci.2024.105337

Web of Science

Scopus

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1299/jtst.23-00279

出版者・発行元：International Journal of Hydrogen Energy  

A flamelet-generated manifold (FGM) method that explicitly considers the preferential diffusion effect, referred to as FGM-PD method, is employed for large-eddy simulations (LESs) of a lean-premixed H2/air low-swirl lifted flame, and the validity is examined by comparing with the experiment. First, the applicability of the FGM-PD method is investigated by one-dimensional numerical simulations of planar laminar premixed H2/air flames. Next, LESs of a lean-premixed H2/air low-swirl lifted flame are performed employing the FGM-PD and conventional FGM methods. Results of the one-dimensional numerical simulations show the importance of considering preferential diffusion to accurately predict species concentrations near the flame front. The FGM-PD method accurately predicts this, and therefore, reproduces the laminar burning velocity and spatial distributions of temperature and mixture fraction. Three-dimensional LES results confirm that the prediction accuracy of the velocities near the flame front is improved by employing this FGM-PD method. Additionally, the OH mass fraction distribution predicted by the FGM-PD method exhibits the inhomogeneous finger-like structure, which has been observed in previous experiments. This inhomogeneity of OH mass fraction distribution, which corresponds to that of the reaction rate, predicted by the FGM-PD method, strongly affects the flame front structure.

DOI： 10.1016/j.ijhydene.2022.12.164

Scopus

出版者・発行元：Physics of Fluids  

Direct numerical simulation is conducted to address the detonation-turbulence interaction in a stoichiometric hydrogen/oxygen/argon mixture. The argon dilution rate is varied so that the mixture composition is 2H2 + O2 + 7Ar and 2H2 + O2 + Ar to discuss the effects of cell regularity on the sensitivity to turbulence. Turbulent Reynolds number and turbulent Mach number are taken to be common for both mixtures. The results show that the shock and flame of detonation in both mixtures are significantly deformed into corrugated ones in the turbulent flow, producing many small unburned gas pockets. However, one-dimensional time-averaged profiles reveal the different sensitivity of the mixtures: in the highly diluted mixture (2H2 + O2 + 7Ar), the reaction progress is not much influenced by turbulence, whereas in the less-diluted mixture (2H2 + O2 + Ar), the reaction takes place more rapidly with turbulence. Analysis of the properties of turbulence and turbulent fluctuations in the detonations clarifies that the direct contribution of turbulence to the flame front is weaker; there is no clear correlation between the heat release and the curvature of the flame. On the other hand, a broader Mach number distribution just upstream of the shock front creates more hot spots in the less-diluted mixture, which results in a shorter induction length. These results indicate that the main contribution of turbulence is creation of different shock strength, which could lead to different reaction rates depending on the cell regularity.

DOI： 10.1063/5.0144624

Scopus

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1063/5.0144624

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.ijhydene.2022.12.164

出版者・発行元：Proceedings of the Combustion Institute  

This work presents a detailed numerical investigation of dilute spray lifted flames experimentally studied by O'Loughlin and Masri at the University of Sydney (O'Loughlin and Masri, Combust. Flame 2011), with a focus on understanding the mechanism that governs flame stabilization under the influence of sprays. Two ethanol flames with varied spray mass loading and degree of partial-premixing at the inlet are simulated by large eddy simulation (LES) combined with the dynamically thickened flame (DTF) model with finite-rate chemistry. Chemical explosive mode analysis (CEMA) is employed which helps identify the prominent role of an entrainment-based ignition process along the shear layer; this process dominates the flame anchoring of the downstream partially-premixed reaction zone. Thus, a higher spray loading can intensify the entrainment, leading to a faster formation of ignition kernels. Furthermore, in present flames, the stabilization point appears to be sustained in a purely gaseous zone with the most reactive mixture fraction and low scalar dissipation rate. Results show that the premixed flamelet can adequately represent flame structures at the leading-edge that are primarily controlled by the inlet partial-premixing, whereas the upstream evolving pre-ignition mixtures are fit for the diffusion flamelet. Moreover, both flamelet configurations fail in capturing downstream structures with a direct spray - flame interaction because the larger droplets produce a less homogeneous mixture with a higher scalar dissipation rate. This is more evident in the lean spray flame.

DOI： 10.1016/j.proci.2022.07.127

Scopus

出版者・発行元：Proceedings of the Combustion Institute  

Large-eddy simulation (LES) employing a flamelet/progress-variable approach that considers the real gas effect is applied to liquid oxygen/ gaseous hydrogen (LOX/GH2) supercritical combustion, and the breakup mechanism of the LOX core is investigated in detail by comparing it to that in the inert case. The results show that in the reactive case, O2 is injected into the chamber in the liquid state; that is, LOX, successively shifts to the supercritical and gas states and then reacts with H2 in the gas state. The present LES in the reactive case generally succeeds in predicting the LOX core breakup location in the experiment. In the reactive case, the LOX core breakup location is observed to be further downstream than in the inert case. This is because in the inert case, the turbulent vortices that are produced around the injector exit act to break the LOX core, whereas in the reactive case, the turbulent vortices are suppressed by the volume dilatation and viscous forces around the LOX core. In the reactive case, the LOX core tends to be compressed and thinned by the thermal expansion caused by the combustion reaction around the LOX core, and at the same time, is stretched and broken by the shear forces caused by the thermal expansion.

DOI： 10.1016/j.proci.2022.07.208

Scopus

記述言語：英語   出版者・発行元：一般社団法人日本機械学会・社団法人日本伝熱学会  

Large-eddy simulation (LES) coupling with a non-adiabatic flamelet progress variable (NA-FPV) approach with reconstructed flamelet chemistry states is employed to simulate the hot coke oven gas (HCOG) reforming process. In the NA-FPV model, the chemistry states are first computed based on the correction factor for enthalpy defects and then modified by substituting the species statistics in the maximum heat loss state with those of less heat release to compensate for the unphysical results. The numerical results of LES coupling this NA-FPV model have been compared with the experimental measurement data in terms of temperature and yields, and reasonable agreements have been achieved. According to the LES results, it is seen O2 only participates in the combustion process in the upper stream and the combustion process which mainly consumes H2 and CO is to provide the other reforming process with heat and steam. In the upper and middle streams, the main HCOG jet is wrapped by the swirling high-temperature combustion products, and the reforming process primarily takes place by consuming CH4, polycyclic aromatic hydrocarbons (PAHs), and steam, while considerable H2, CO, and CO2 are produced. It is observed that accompanying the reforming process C2H2 is generated and it peaks in the middle stream, thus it is considered soot is formed in the complex reactions.

DOI： 10.1299/jtst.23-00279

Web of Science

Scopus

CiNii Research

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.jaecs.2022.100083

出版者・発行元：Applications in Energy and Combustion Science  

Large eddy simulation (LES) employing a flamelet model coupled with an artificial neural network (ANN), namely the LES/flamelet/ANN is developed for supercritical oxy-fuel combustion and its validity is investigated in detail. An ANN is introduced to reduce the size of the flamelet library for non-adiabatic three gas-stream conditions of a real supercritical carbon dioxide (CO2) combustor. The fuel and oxidizer are methane (CH4) and a mixture of oxygen (O2) and CO2, respectively. To consider the real gas effect, the Soave-Redlich-Kwong (SRK) equation of state is solved to generate the flamelet library. The LES/flamelet/ANN is applied to two combustion fields in the combustor, namely the upstream and full fields of the combustor with low and high mesh sizes, respectively. The LES/flamelet/ANN for the upstream field is conducted to examine its applicability to the non-adiabatic three gas streams condition by varying the resolution of the flamelet library and by comparing it with the results obtained by the conventional LES/flamelet. The LES/flamelet/ANN for the full field is also conducted to validate the approach by comparing its results with those obtained from the experiment. The results show that the LES/flamelet/ANN of the upstream field properly reproduces the supercritical combustion behavior generated by the conventional LES/flamelet while maintaining the same level of computational cost. Furthermore, the LES/flamelet/ANN for the full field reasonably predicts the supercritical combustion behavior in the experiment, and the predicted combustor outlet temperature agrees well with the experimental results.

DOI： 10.1016/j.jaecs.2022.100083

Scopus

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1080/00102202.2022.2150971

記述言語：英語   掲載種別：研究論文（国際会議プロシーディングス）  

DOI： https://doi.org/10.1016/j.proci.2022.07.208

記述言語：英語   掲載種別：研究論文（国際会議プロシーディングス）  

DOI： https://doi.org/10.1016/j.proci.2022.07.127

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.combustflame.2021.111615

出版者・発行元：Combustion and Flame  

Design of Compression Ignition (CI) engines with improved thermal efficiencies needs better understanding of the heat transfer mechanism from spray flame to the combustion chamber wall. In this regard, heat transfer occurring during the interaction between impinging spray flame and wall, under CI engine-like conditions, is investigated in this study using 3-Dimensional numerical simulations based on an Eulerian–Lagrangian framework. Simulations are performed for different fuel spray injection velocities (which are representative of different fuel injection pressures in CI engines), to examine their influence on the heat transfer between impinging spray flame and wall. To couple the convective and radiative heat transfer at the wall surface with the conduction heat transfer occurring within the finite thickness wall, Conjugate Heat Transfer (CHT) is incorporated in the simulations. A Non-Adiabatic Flamelet/Progress Variable (NA-FPV) approach is employed as the combustion model of n-dodecane, which is considered to be the fuel for liquid spray. Dynamics of the liquid film formed on the wall surface by impinging fuel droplets are captured using a particle-based approach. Contribution of radiative heat flux is taken into consideration using the Discrete Ordinates (DO) method. Results indicate that the total heat flux (sum of convective and radiative heat fluxes) at the wall surface increases with the fuel injection velocity. It is observed that the total wall heat flux is largest in the stagnation zone where the spray flame impinges directly on the wall surface, while the radiative heat flux at the wall surface becomes larger as the distance from this stagnation zone increases. Additionally, it is found that the influence of fuel injection velocity on the radiative heat flow rate at the wall surface is rather small. This radiative heat flow rate when expressed as a percentage of the total wall heat flow rate, ranges from ≈ 18% to 30% (depending on the 3 cases investigated), indicating that its contribution cannot be neglected for the CI engine-like conditions under which the present simulations are performed. Furthermore, to characterize the heat transfer occurring during spray flame-wall interaction process, correlations between the Nusselt number Nu (corresponding to the wall heat loss) and Reynolds number Re (of the flow field) of the form Nu∝Ren, are analysed and compared with that of a previous experimental study to assess their applicability. It is found that, depending on how the Nusselt number Nu is defined (either using the total wall heat flux or the convective heat flux), the value of the correlation index n changes. When Nu is calculated based on the total wall heat flux (which includes the contribution from the radiative heat flux), the value of n is found to be 0.49 which is close to the correlation index value of n=0.4 reported in the recent experiments performed at Toyota Central R&D Labs., Inc.

DOI： 10.1016/j.combustflame.2021.111615

Scopus

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.energy.2021.121352

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.egyai.2021.100076

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.jaecs.2020.100022

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.38036/jgpp.11.3_8

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1299/jtst.2020jtst0033

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.applthermaleng.2020.115947

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.ijmultiphaseflow.2020.103216

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.jngse.2020.103158

記述言語：英語   掲載種別：研究論文（学術雑誌）  

DOI： https://doi.org/10.1016/j.energy.2019.07.101

開催年月日： 2023年11月 - 2023年12月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2023年11月 - 2023年12月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2023年11月

記述言語：英語   会議種別：口頭発表（一般）  

国名：アメリカ合衆国  

開催年月日： 2023年11月

記述言語：英語   会議種別：口頭発表（一般）  

国名：アメリカ合衆国  

開催年月日： 2023年11月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：秋田アトリオン（秋田市）   国名：日本国  

開催年月日： 2023年11月

記述言語：日本語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2023年11月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：秋田アトリオン（秋田市）   国名：日本国  

開催年月日： 2023年10月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：神戸大学大学院工学研究科（神戸市）   国名：日本国  

開催年月日： 2023年10月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：福井県国際交流会館（福井市）   国名：日本国  

開催年月日： 2023年10月

記述言語：日本語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2023年9月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：東京農工大学小金井キャンパス（小金井市）   国名：日本国  

開催年月日： 2023年9月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：東京農工大学小金井キャンパス（小金井市）   国名：日本国  

開催年月日： 2023年9月

記述言語：英語   会議種別：口頭発表（一般）  

国名：イタリア共和国  

開催年月日： 2023年7月

記述言語：英語   会議種別：口頭発表（一般）  

国名：大韓民国  

開催年月日： 2023年7月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2023年5月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2023年3月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2023年3月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2023年3月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：産業技術総合研究所つくば中央共用講堂（茨城県）   国名：日本国  

開催年月日： 2022年12月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：オンライン   国名：日本国  

開催年月日： 2022年11月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：KFC Hall & Rooms（東京都）   国名：日本国  

開催年月日： 2022年11月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：KFC Hall & Rooms（東京都）   国名：日本国  

開催年月日： 2022年11月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：熊本大学 工学部2号館（熊本県）   国名：日本国  

開催年月日： 2022年10月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：九州大学医学部　百年講堂（福岡県）   国名：日本国  

開催年月日： 2022年9月

記述言語：英語   会議種別：口頭発表（一般）  

開催年月日： 2022年3月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：米子コンベンションセンター（鳥取県）   国名：日本国  

開催年月日： 2021年12月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：オンライン   国名：日本国  

開催年月日： 2021年11月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：オンライン   国名：日本国  

開催年月日： 2021年10月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：オンライン   国名：日本国  

開催年月日： 2021年10月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2021年9月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：オンライン   国名：日本国  

開催年月日： 2021年8月 - 2021年9月

記述言語：英語   会議種別：口頭発表（一般）  

開催年月日： 2020年12月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：オンライン   国名：日本国  

開催年月日： 2020年10月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：オンライン   国名：日本国  

開催年月日： 2020年9月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：オンライン   国名：日本国  

開催年月日： 2019年11月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2019年11月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2019年11月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2019年9月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：電気通信大学（東京都）   国名：日本国  

開催年月日： 2019年7月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2019年7月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2019年5月

記述言語：英語   会議種別：口頭発表（一般）  

国名：ドイツ連邦共和国  

開催年月日： 2019年2月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国  

開催年月日： 2018年11月

記述言語：英語   会議種別：口頭発表（一般）  

開催年月日： 2018年11月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：堺市産業振興センター（大阪府）   国名：日本国  

開催年月日： 2018年11月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：堺市産業振興センター（大阪府）   国名：日本国  

開催年月日： 2018年8月

記述言語：英語   会議種別：口頭発表（一般）  

国名：中華人民共和国  

開催年月日： 2018年6月

記述言語：英語   会議種別：口頭発表（一般）  

開催年月日： 2017年12月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：京都工芸繊維大学（京都府）   国名：日本国  

開催年月日： 2017年11月

記述言語：英語   会議種別：口頭発表（一般）  

開催年月日： 2017年11月

記述言語：日本語   会議種別：口頭発表（一般）  

開催地：富山国際会議場（富山県）   国名：日本国  

開催年月日： 2017年10月

記述言語：英語   会議種別：口頭発表（一般）  

国名：日本国