Flutter Analysis of Aircraft Wing Using an Alternative Reduced-Order Modelling Method. International Conference on Power Electronics and Energy Engineering, 98-101.
Optimal synthesis of four-bar linkage path generation through evolutionary computation. Research and Applications in Mechanical Engineering 3(2), 46-53.
Morphing Wing Structural Optimization Using Opposite-Based Population-Based Incremental Learning and Multigrid Ground Elements. Mathematical Problems in Engineering Article ID 730626.
Multiobjective Optimization of a Steering Linkage. Journal of Mechanical Science and Technology 30 (8), 3681-3691.
Four-bar linkage path synthesis using meta-heuristics-algorithm comparison. Paper presented at the seventh TSME – ICOME, Chiang Mai, 2016 Thailand.
Four-bar linkage path generation through self-adaptive population size teaching-learning based optimization. Knowledge-Based Systems 135, 180-191.
Topology optimisation using MPBILs and multi-grid ground element. Applied Sciences 8 (2), art. no. 271.
Alternative Constraint Handling Technique for Four-Bar Linkage Path Generation. IOP Conf Series: Mater Sci Eng, 324, 012012.
Optimal Synthesis of Four-Bar Linkage Path Generation through Evolutionary Computation with a Novel Constraint Handling Technique. Computational Intelligence and Neuroscience, Vol. 2018, Article ID 5462563.
Vibration Suppression of a Single-Cylinder Engine by Means of Multi-objective Evolutionary Optimisation. Sustainability 10(6), Article ID 2067
Investigation of cooling performances of a non-film-cooled turbine vane coated with a thermal barrier coating using conjugate heat transfer. Energies 11 (4), 1000
Alternative Constraint Handling Technique for Four-Bar Linkage Motion Generation. IOP Conf Series: Mater Sci Eng, 501, 012042.
Synthesis of four-bar linkage motion generation using optimization algorithms. Advances in Computational Design 4(3), 197-210.
Numerically thermal analysis of a turbine vane at high temperature. Journal of Physics: Conference Series 1369 (1), Article id. 012001
CHT/CFD Analysis of Thermal Sensitivity of a Transonic Film-Cooled Guide Vane, CMES-COMPUTER MODELING IN ENGINEERING & SCIENCES119(3), 593-615.
High-Lift Mechanism Motion Generation Synthesis Using a Metaheuristic. Multidisciplinary Digital Publishing Institute Proceedings 39 (1), Article no. 5
Surrogate-Assisted Reliability Optimisation of an Aircraft Wing with Static and Dynamic Aeroelastic Constraints. International Journal of Aeronautical and Space Sciences 21, 723–732.
Reliability-Based Design Optimization of Classical Wing Aeroelasticity IOP Conf. Series: Materials Science and Engineering 886 (1), 012015.
Constraint handling technique for four-bar linkage path generation using self-adaptive teaching–learning-based optimization with a diversity archive. Engineering Optimization 53 (3), 513-530
Multi-objective Reliability-based Topology Optimization of Structures Using a Fuzzy Set Model. Journal of Mechanical Science and Technology 34(10), 3973-3980.
Multi-objective, Reliability-based Design Optimization of a Steering Linkage. Applied Science 10(17), 5748.
Constraint handling technique for four-bar linkage path generation using self-adaptive teaching–learning-based optimization with a diversity archive.Engineering Optimization, 53 (3), 513-530.
Optimization of a High-Lift Mechanism Motion Generation Synthesis Using MHS. Lecture Notes in Computer Science, vol 12689, 38-45.
Reliability-Based Design of an Aircraft Wing Using a Fuzzy-Based Metaheuristic. Appl. Sci. 11, 6463.
Ground Structures-Based Topology Optimization of a Morphing Wing Using a Metaheuristic Algorithm. Metals., 11(8):1311.
Reduced-order modelling of unsteady vortex lattice method. IOP Conference Series: Materials Science and Engineering 1173 (1), 012040.
“Deep Neural Learning Adaptive Sequential Monte Carlo for Automatic Image and Speech Recognition”, Applied Computational Intelligence and Soft Computing, vol. 2020, Article ID 8866259, 9 pages, 2020. https://doi.org/10.1155/2020/8866259
Vision-Based Spacecraft Pose Estimation via a Deep Convolutional Neural Network for Noncooperative Docking Operations. Aerospace 2020, 7, 126.
An enhanced learning algorithm with a particle filter-based gradient descent optimizer method. Neural Comput and Applic (2020). https://doi.org/10.1007/s00521-020-04726-9
The dynamics of wetland cover change using a state estimation technique applied to time-series remote sensing imagery, Geomatics, Natural Hazards and Risk, 8:2, 1662-1677, DOI: 10.1080/19475705.2017.1370025
“A Support Vector Machine-Based Particle Filter Method for Improved Flooding Classification,” in Geoscience and Remote Sensing Letters, IEEE, vol.12, no.9, pp.1943-1947, Sept. 2015. doi: 10.1109/LGRS.2015.2439575.
“Joint iterative channel estimation and decoding under impulsive interference condition,” in ICACT Transactions on the Advanced Communications Technology (TACT), GIRI (Global IT Research Institute), Vol. 4, Issue 4, pp.636-643, July 2015. ISSN: 2288-0003.
“Wi-Fi Received Signal Strength-based Indoor Localization System Using K-Nearest Neighbors fingerprint integrated D*algorithm,” 2021 23rd International Conference on Advanced Communication Technology (ICACT), PyeongChang, Korea (South), 2021, pp. 242-247, doi: 10.23919/ICACT51234.2021.9370734
“Cooperative Motion Planning for Multiple UAVs via the Bézier Curve Guided Line of Sight Techniques,” 2021 23rd International Conference on Advanced Communication Technology (ICACT), PyeongChang, Korea (South), 2021, pp. 230-236, doi: 10.23919/ICACT51234.2021.9370684.
“Aircraft trajectory recognition via statistical analysis clustering for Suvarnabhumi International Airport,” 2020 22nd International Conference on Advanced Communication Technology (ICACT), Phoenix Park, PyeongChang, Korea (South), 2020, pp. 290-297, doi: 10.23919/ICACT48636.2020.9061368.
“Vision-based attitude estimation for spacecraft docking operation through deep learning algorithm,” 2020 22nd International Conference on Advanced Communication Technology (ICACT), Phoenix Park, PyeongChang, Korea (South), 2020, pp. 280-284, doi: 10.23919/ICACT48636.2020.9061445.
Enhancing the Capability of a Ground-Based Optical Telescope for Thai National Space Objects Observation. Proceedings 2019, 39, 15. https://doi.org/10.3390/proceedings2019039015
“Deep Convolutional Neural Networks for plane identification on Satellite imagery by exploiting transfer learning with a different optimizer,” IGARSS 2019 – 2019 IEEE International Geoscience and Remote Sensing Symposium, Yokohama, Japan, 2019, pp. 9788-9791.doi: 10.1109/IGARSS.2019.8899206
“A support vector machine-based particle filter for improved land cover classification applied to MODIS data,” 2016 IEEE International Geoscience and Remote Sensing Symposium (IGARSS), Beijing, 2016, pp. 775-778. doi: 10.1109/IGARSS.2016.7729195.
“Joint iterative channel estimation and decoding under impulsive interference condition,” 2016 18th International Conference on Advanced Communication Technology (ICACT), Pyeongchang Kwangwoon Do, South Korea, 2016, pp. 636-643. doi: 10.1109/ICACT.2016.7423585
“Joint iterative channel estimation and decoding under pulsed radio frequency interference condition,” Advanced Communication Technology (ICACT), 2014 16th International Conference on, Pyeongchang, 2014, pp. 983-988. doi: 10.1109/ICACT.2014.6779105
Experimental Study of a NACA0015 Circulation Control Airfoil Using Synthetic Jet Actuation. AIAA Journal. In press.
Spectral Analysis of Unsteady Shear Flows over a Rounded-Trailing-Edge Airfoil. Journal of Aircraft.
Large Eddy Simulation of a NACA0015 Circulation Control Airfoil Using Synthetic Jets. Aerospace Science and Technology.
Numerical Study of a NACA0015 Circulation Control Aerofoil Using Synthetic Jets. 21st Australasian Fluid Mechanics Conference.
Experimental Study of a NACA0015 Circulation Control Aerofoil Using Synthetic Jets. 9th Asia-Pacific Conference on Wind Engineering.
Toward the Design of a Synthetic Jet Actuator for use on a Circulation Control Aerofoil and Its Bench Top Characterisation. 20th Australasian Fluid Mechanics Conference.
NACA0015 Circulation Control Airfoil Using Synthetic Jets at Low Angles of Attack and Low Reynolds Number. 8th AIAA Flow Control Conference. AIAA Paper 2016-3772.
“Predicting adiabatic film effectiveness of a turbine vane by two-equation turbulence models,” The 60th ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, June 15-19, Montreal, Canada.
“Film cooling performances at different turbulence intensities using conjugate heat transfer analysis,” The 2nd International Conference on Applied Engineering, Materials and Mechanics 2017, April 14-16, 2017, Tianjin, China.
“Extra-low Reynolds number vane separation using immersed boundary method,” The ASME-JSME-KSME 2019: Joint Fluids Engineering Conference AJKFLUIDS2019, July 28-August 1, 2019, San Francisco, CA, USA.
“Numerically thermal analysis of a turbine vane at high temperature,” The 5th International Workshop on Heat/Mass Transfer Advances for Energy Conservation and Pollution Control, August 13-16, 2019, Novosibirsk, Russia.
“Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions,” The ASME 2019: Gas Turbine India Conference GTINDIA2019, December 5-6, 2019, Chennai, India.
“Investigation of flexibility effect on the aerodynamics of insect wing in complicated environment,” The 10th Asian-Pacific Conference on Aerospace Technology and Science & The 4th Asian Joint Symposium on Aerospace Engineering, August 28-31, 2019, Hsin Chu, Taiwan.
“Parametric study on wing-lambda-shock formation,” The ASME 2021: Fluids Engineering Division Summer Meeting FEDSM 2021, August 10-12, 2021, Virtual conference.
“Influence of coolant on cooling performance sensitivity of internally convective turbine vane,” The ASME 2021: Gas Turbine India Conference GTINDIA2021, December 2–3, 2021, Virtual conference.
“Predicting adiabatic film effectiveness of a turbine vane by two-equation turbulence models,” The Proceedings of ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, Vol. 5B, GT2015-42565. (WOS/SCOPUS)
“Thermal barrier coating and turbulence intensity effects on leading edge cooling using conjugate heat transfer analysis,” Transactions of the Canadian Society for Mechanical Engineering, 2017, Vol. 41, No. 2, pp. 249-263. (SCIE/SCOPUS)
“Numerical study of the effects of thermal barrier coating and turbulence intensity on cooling performances of a nozzle guide vane,” Energies, 2017, Vol. 10(3), pp. 362. (SCIE/SCOPUS)
“Film cooling performances at different turbulence intensities using conjugate heat transfer analysis,” Applied Mechanics and Materials, 2017, Vol. 872, pp. 271-278. (SCOPUS/EI)
“Investigation of cooling performances of a non-film-cooled turbine vane coated with a thermal barrier coating using conjugate heat transfer,” Energies, 2018, Vol. 11(4), pp. 1000. (SCIE/SCOPUS)
“CHT/CFD analysis of thermal sensitivity of a transonic film-cooled guide vane,” Computer Modeling in Engineering & Sciences, 2019, Vol. 119, No. 3, pp. 593-615. (SCIE/SCOPUS)
“Numerically thermal analysis of a turbine vane at high temperature,” Journal of Physics: Conference Series, 2019, Vol. 1369, pp. 012001. (WOS/SCOPUS)
“Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions, The proceedings of the ASME 2019: Gas Turbine India Conference GTINDIA 2019, Vol. 1, GTINDIA2019-2628. (WOS/SCOPUS)
“Understanding of temperature and cooling effectiveness sensitivity of a film-cooled vane under coolant inlet temperature effect: a case study,” Case Studies in Thermal Engineering, 2019, Vol. 14, pp. 100505. (WOS/SCOPUS)
“Separate and combined effects of surface roughness and thermal barrier coating on vane cooling performance,” Journal of Thermal Science and Engineering Application: ASME, 2020, 12(5): 051017 (SCIE/SCOPUS)
“Influence of coolant on cooling performance sensitivity of internally convective turbine vane,” The proceedings of the ASME 2021: Gas Turbine India Conference GTINDIA2021, GTINDIA2021-76021. (WOS/SCOPUS) (Accepted)
“Extra-low Reynolds number vane separation using immersed boundary method,” The Proceedings of the ASME-JSME-KSME 2019 Joint Fluids Engineering Conference AJKFLUIDS2019, Vol. 2, AJKFLUIDS2019-5077. (WOS/Scopus)
“Finite obstacle effect on the aerodynamic performance of a hovering wing,” Physics of Fluids, 2019, Vol. 31, pp. 101902. (SCIE/SCOPUS)
“Multi-objective design optimization of the combinational the upstream energy deposition and opposing jet configuration for drag reduction in supersonic flows,” Aerospace Science and Technology 2020, 105, 105941 (SCIE/SCOPUS)
“Parametric study on drag reduction with the combinational the upstream energy deposition and opposing jet configuration in supersonic flows,” Acta Astronautica 2020, Vol. 171, pp. 300-310. (SCIE/SCOPUS)
“Recent progress in flexibility effects on wing aerodynamics and acoustics,” Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 2021, Vol. 235(2), pp. 208-244. (SCIE/SCOPUS)
“Parametric study on wing-lambda-shock formation,” The Proceedings of the ASME 2021: Fluids Engineering Division Summer Meeting FEDSM 2021, FEDSM2021- 60958. (WOS/SCOPUS) (In press)
“High Voltage Plasma Using Pulsed Direct Coil”, The 3rd International workshop on advanced plasma technology and applications, 11-14 Jan., 2017, Ho chi Minh city, Vietnam.
“Grain size dependence of penetration depth of hydrogen injection into polycristalline tungsten by binarycollision-approximation-based simulation” ISPlasma 2017/IC-PLANTS2017, March 1-5, 2017.
“Investigation of Cooling Performances of a non-Film-Cooled Turbine Vane Coated with a Thermal Barrier Coating Using Conjugate Heat Transfer”, 2018, Energies, 11,1000.
“Effect of polycrystalline structure on helium plasma irradiation of tungsten materials”, 2018, Japanese Journal of Applied Physics, Volume 57, Number 1S.
“CHT/CFD “Predictions of Thermal Sensitivity of a Film-Cooled Turbine Vane Coated with Thermal Barrier at Different Turbulence Intensities”, 2018, Iranian Journal of Science and Technology: Transactions of Mechanical Engineering.
Investigation of Cooling Performances of a Non-Film-Cooled Turbine Vane Coated with a Thermal Barrier Coating Using Conjugate Heat Transfer Energies, 2018; 11, art. no. 1000.
CHT/CFD Analysis of Thermal Sensitivity of a Transonic Film-Cooled Guide Vane, Cmes-Computer Modeling In Engineering & Sciences, 2019; 119 (3), 593-615.
Numerically thermal analysis of a turbine vane at high temperature. JPCS, 2019; 1369 (1), 012001.
“Deep Convolutional Neural Networks for plane identification on Satellite imagery by exploiting transfer learning with a different optimizer”, 2019, The 39th annual IGARSS IEEE symposium. July 28th, August 1-3, 2019, Japan.
“Influence of the trailing edge shape on the aerodynamic characteristics of an airfoil at low Re number using RANS” TSMEICOME 2019, Pattaya, Thailand, Dec. 10th-13th 2019.
“Deep Convolutional Neural Networks for plane identification on Satellite imagery by exploiting transfer learning with a different optimizer,” IGARSS 2019 – 2019 IEEE International Geoscience and Remote Sensing Symposium, Yokohama, Japan, 2019, pp. 9788-9791. doi: 10.1109/IGARSS.2019.8899206.
Perceptions of Thai Aviation Students on Consumer Grade VR Flight Experiences, Proceeding 2019,39(1), https://doi.org/10.3390/proceedings2019039008 – 31 Dec 2019.
A Novel Stress Tensor- Based Failure Criterion for Peridynamics, Proceedings 2019,39(1), 23 ; https://doi.org/10.3390/proceedings2019039023 – 09 Jan 2020.
“Aircraft trajectory recognition via statistical analysis clustering for Suvarnabhumi International Airport,” 22nd International Conference on Advanced Communication Technology, Pyeongchang, 2020, pp. 290-297.
“Vision-based attitude estimation for spacecraft docking operation through deep learning algorithm,” 22nd International Conference on Advanced Communication Technology, Pyeongchang, 2020, pp. 280-284.
An enhanced learning algorithm with a particle filter-based gradient descent optimizer method. Neural Comput & Applic (2020). https://doi.org/10.1007/s00521-020-04726-9.
Efficacy of Ultraviolet Radiation on Microbial Eliminations from Conditioning Airflow, Published: 03 July 2021 by MDPI in Innovation Aviation & Aerospace Industry – International Conference 2021 session Applied Sciences and Engineering DOI.10.3390/IAAI-2021-10599
