Pub Date : 2021-10-01DOI: 10.1109/ICMEAS54189.2021.00025
E. Marakhova, A.B. Shimanova, D. Uglanov, H. Adenane
In nowadays the best way to carry an operating body such hydrogen or nitrogen for example it’s to carry it in liquid state and low temperature which is cryogenic state. In this work it will be shown a computational studies of the recondensation process in a tank with a cryogenic filling, and also a promising technologies in the cryogenic filling tank that have been realized at the laboratory of Samara University. The computational studies carried out allow us to draw the following conclusion that during regasification of a cryoproduct in the cryogenic filling tank, recondensation of a part of the gasified product occurs due to the temperature difference between the wall of the thermos and the inner wall of the cryogenic filling tank. This process is observed at the beginning of regasification (in the first 3-5 minutes), and the intensity of this process is low and amounts to about 2-8%.
{"title":"Computational Studies of the Recondensation Process in a Tank with a Cryogenic Filling","authors":"E. Marakhova, A.B. Shimanova, D. Uglanov, H. Adenane","doi":"10.1109/ICMEAS54189.2021.00025","DOIUrl":"https://doi.org/10.1109/ICMEAS54189.2021.00025","url":null,"abstract":"In nowadays the best way to carry an operating body such hydrogen or nitrogen for example it’s to carry it in liquid state and low temperature which is cryogenic state. In this work it will be shown a computational studies of the recondensation process in a tank with a cryogenic filling, and also a promising technologies in the cryogenic filling tank that have been realized at the laboratory of Samara University. The computational studies carried out allow us to draw the following conclusion that during regasification of a cryoproduct in the cryogenic filling tank, recondensation of a part of the gasified product occurs due to the temperature difference between the wall of the thermos and the inner wall of the cryogenic filling tank. This process is observed at the beginning of regasification (in the first 3-5 minutes), and the intensity of this process is low and amounts to about 2-8%.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122063290","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2021-10-01DOI: 10.1109/icmeas54189.2021.00022
F. Meng, DashunZhang, Jing Wang, Liqin Miao, Xueguang Li, Huizhong Hu
This electronic With the rapid development of global knowledge economy and science & technology, virtual manufacturing technology based on virtual reality and simulation technology came into being. The Virtual Machine Tool (VMT), as the execution unit of virtual manufacturing, is a key technology and prerequisite for virtual manufacturing. This article uses UG software to complete the construction of the geometric model of the three-axis CNC machine tool, and the NC machining program of the machined parts is generated based on UG CAM. By acquiring the actual machine structure, import the geometric model established in UG into VERICUT to create the kinematic model of the virtual machine tool. Taking a certain type of flange as the simulation processing object, and use the NC program generated in UG CAM to processing simulation in VERICUT. This verifies the correctness of the established model and NC program. Through optimizing the NC machining parameters, the collision or interference between machine tools and parts in actual processing can be avoided.
{"title":"Simulation Verification of Parts Processing Based on Virtual Numerical Control Machine","authors":"F. Meng, DashunZhang, Jing Wang, Liqin Miao, Xueguang Li, Huizhong Hu","doi":"10.1109/icmeas54189.2021.00022","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00022","url":null,"abstract":"This electronic With the rapid development of global knowledge economy and science & technology, virtual manufacturing technology based on virtual reality and simulation technology came into being. The Virtual Machine Tool (VMT), as the execution unit of virtual manufacturing, is a key technology and prerequisite for virtual manufacturing. This article uses UG software to complete the construction of the geometric model of the three-axis CNC machine tool, and the NC machining program of the machined parts is generated based on UG CAM. By acquiring the actual machine structure, import the geometric model established in UG into VERICUT to create the kinematic model of the virtual machine tool. Taking a certain type of flange as the simulation processing object, and use the NC program generated in UG CAM to processing simulation in VERICUT. This verifies the correctness of the established model and NC program. Through optimizing the NC machining parameters, the collision or interference between machine tools and parts in actual processing can be avoided.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"40 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"117049773","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
With the improvement of the complexity of civil aircraft,Model Based Systems Engineering(MBSE) plays more important role in the aircraft design nowadays. In this paper, an architecture design method based on MBSE applied in aircraft cabin pressure control system is introduced. A top-down design process including functional physical architecture analysis is presented to ensure final solution can meet stakeholder needs. Functional architecture produced by functional analysis which transfers stakeholder needs and top-level requirements to design requirements has great effects on physical solution design. Physical architecture which is implementation of functional architecture provides enough detail to synthesize a physical architecture. This paper proposes a framework for efficient architecture based MBSE which can also provide common understanding of the scope and characterization of the system for engineers involved in system design. It shows that the proposed MBSE method significantly improves synthesis of design and integration, and ensure the requirements can be properly implemented
{"title":"Application Practice of Model-Based System Engineering Method in Civil Aircraft Cabin Pressure Control System Design","authors":"Tang Chao, He Yan, Zhang Kaili, litao litao, Jiafeng Li, Zhang Xinai","doi":"10.1109/icmeas54189.2021.00045","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00045","url":null,"abstract":"With the improvement of the complexity of civil aircraft,Model Based Systems Engineering(MBSE) plays more important role in the aircraft design nowadays. In this paper, an architecture design method based on MBSE applied in aircraft cabin pressure control system is introduced. A top-down design process including functional physical architecture analysis is presented to ensure final solution can meet stakeholder needs. Functional architecture produced by functional analysis which transfers stakeholder needs and top-level requirements to design requirements has great effects on physical solution design. Physical architecture which is implementation of functional architecture provides enough detail to synthesize a physical architecture. This paper proposes a framework for efficient architecture based MBSE which can also provide common understanding of the scope and characterization of the system for engineers involved in system design. It shows that the proposed MBSE method significantly improves synthesis of design and integration, and ensure the requirements can be properly implemented","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"37 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"117000765","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2021-10-01DOI: 10.1109/icmeas54189.2021.00032
Liu Jingwei, Lin Jiaming
Dual engine failure is the most serious risk that a civil airplane may encounter in airline operations and flight tests. CCAR-25.671(d) clearly stipulates that the airplane must be designed so that it is controllable if all engines fail. In this paper, by building the aircraft 6-DOF motion simulation model and the control surface malfunction simulation model, the theoretical calculation and analysis of the airplane control characteristics after dual engine failure are given. Moreover, the safety of civil airplane under dual engine failure condition is evaluated. Finally, reasonable suggestions are given based on engineering experience, which can provide a reference for dual engine failure flight test of civil aircraft.
{"title":"Research on Handling Risk Assessment for Civil Airplane under Dual Engine Failure","authors":"Liu Jingwei, Lin Jiaming","doi":"10.1109/icmeas54189.2021.00032","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00032","url":null,"abstract":"Dual engine failure is the most serious risk that a civil airplane may encounter in airline operations and flight tests. CCAR-25.671(d) clearly stipulates that the airplane must be designed so that it is controllable if all engines fail. In this paper, by building the aircraft 6-DOF motion simulation model and the control surface malfunction simulation model, the theoretical calculation and analysis of the airplane control characteristics after dual engine failure are given. Moreover, the safety of civil airplane under dual engine failure condition is evaluated. Finally, reasonable suggestions are given based on engineering experience, which can provide a reference for dual engine failure flight test of civil aircraft.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":" 36","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132012224","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2021-10-01DOI: 10.1109/icmeas54189.2021.00043
Norfarahana Adibah Raffie, N. H. Amer, Syed Mohd Fairuz Syed Mohd Dardin, K. Hudha, S. Ishak
Hazardous environments gave a big challenge for the human to accomplish the desired tasks, especially in sampling and collecting materials either for securing the locality or research purposes. Hence, teleoperated robots with robotic arms have been proposed to execute any tasks that appointed. However, most robotic arms on the teleoperated robots only serve specific tasks and have no ability to retract arm with precise and smooth movement, which will compromise its functionality. In this paper, five designs of robotic arms were proposed with different mechanisms for its retractions. Evaluation and selection for the final design was decided based on the decision-making process for all designs. Considering important criterion, evaluation was performed using concept scoring. All concept designs were modelled and analysed in SolidWorks. Load was applied on the end effector of robotic arm to observe Von Mises criteria of designed arms. Both methods indicate that design 5 with linear motor mechanism has the best endurance and thus, chosen as the most suitable design to be mounted on the track vehicle.
{"title":"Preliminary Concept Modelling, Evaluation and Selection of Robotic Arm for Light Lifting Application","authors":"Norfarahana Adibah Raffie, N. H. Amer, Syed Mohd Fairuz Syed Mohd Dardin, K. Hudha, S. Ishak","doi":"10.1109/icmeas54189.2021.00043","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00043","url":null,"abstract":"Hazardous environments gave a big challenge for the human to accomplish the desired tasks, especially in sampling and collecting materials either for securing the locality or research purposes. Hence, teleoperated robots with robotic arms have been proposed to execute any tasks that appointed. However, most robotic arms on the teleoperated robots only serve specific tasks and have no ability to retract arm with precise and smooth movement, which will compromise its functionality. In this paper, five designs of robotic arms were proposed with different mechanisms for its retractions. Evaluation and selection for the final design was decided based on the decision-making process for all designs. Considering important criterion, evaluation was performed using concept scoring. All concept designs were modelled and analysed in SolidWorks. Load was applied on the end effector of robotic arm to observe Von Mises criteria of designed arms. Both methods indicate that design 5 with linear motor mechanism has the best endurance and thus, chosen as the most suitable design to be mounted on the track vehicle.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"49 3-4 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123456739","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2021-10-01DOI: 10.1109/icmeas54189.2021.00029
Jihong Yan, Xiaofeng Wang, Ahad Ali
Tool wear monitoring is the key part of intelligent maintenance and has been attracting considerable interest. However, traditional data-driven methods assume that the collected data following identical distribution and the training data is sufficient, which is impractical in practice. This paper proposed a novel framework to realize tool wear monitoring across scenarios based on deep transfer learning. The collected multi-source heterogeneous signal is fused based on the feature self-extraction and selection capabilities of deep learning. Particularly, the feature extraction capability of convolutional neural networks (CNN) for structured data is improved by integrating traditional feature extraction methods. Furthermore, the transfer learning technique is introduced to migrate the pre-trained model from the source domain to the target domain, and thus achieving the tool wear monitoring across scenarios. The proposed framework was applied to the continuous cutting process of tools and the excellent experimental results demonstrated the effectiveness of the deep transfer learning network for tool wear monitoring with a small number of labeled data, which demonstrates the practicality of the proposed framework.
{"title":"Deep Transfer Learning Based Multi-source Heterogeneous data Fusion with Application to Cross-scenario Tool Wear monitoring","authors":"Jihong Yan, Xiaofeng Wang, Ahad Ali","doi":"10.1109/icmeas54189.2021.00029","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00029","url":null,"abstract":"Tool wear monitoring is the key part of intelligent maintenance and has been attracting considerable interest. However, traditional data-driven methods assume that the collected data following identical distribution and the training data is sufficient, which is impractical in practice. This paper proposed a novel framework to realize tool wear monitoring across scenarios based on deep transfer learning. The collected multi-source heterogeneous signal is fused based on the feature self-extraction and selection capabilities of deep learning. Particularly, the feature extraction capability of convolutional neural networks (CNN) for structured data is improved by integrating traditional feature extraction methods. Furthermore, the transfer learning technique is introduced to migrate the pre-trained model from the source domain to the target domain, and thus achieving the tool wear monitoring across scenarios. The proposed framework was applied to the continuous cutting process of tools and the excellent experimental results demonstrated the effectiveness of the deep transfer learning network for tool wear monitoring with a small number of labeled data, which demonstrates the practicality of the proposed framework.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"28 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126210858","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2021-10-01DOI: 10.1109/icmeas54189.2021.00014
Qian Pengjun, Lu Zhengliang
This article addresses the attitude stabilization control problem of the moving mass rocket-propelled CubeSat in orbit maneuver. Considering the propellant combustion and the motion of two moving masses, the attitude dynamic model of the satellite is established by Newton multi-rigid system with variable mass dynamic. Subsequently, based on the simplified control model of pitch and yaw channel, backstepping technique is utilized to design the controller and the dynamic surface control is employed to avoid the computer explosion. An adaptive law is proposed to estimate the upper boundaries of uncertainties. Lyapunov function is used to prove the stability of the closed-loop system. Finally, numerical simulation results indicate the effectiveness of the designed control method.
{"title":"Adaptive Backstepping Terminal Sliding Mode Attitude stabilization control for Moving Mass Rocket-propelled CubeSat","authors":"Qian Pengjun, Lu Zhengliang","doi":"10.1109/icmeas54189.2021.00014","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00014","url":null,"abstract":"This article addresses the attitude stabilization control problem of the moving mass rocket-propelled CubeSat in orbit maneuver. Considering the propellant combustion and the motion of two moving masses, the attitude dynamic model of the satellite is established by Newton multi-rigid system with variable mass dynamic. Subsequently, based on the simplified control model of pitch and yaw channel, backstepping technique is utilized to design the controller and the dynamic surface control is employed to avoid the computer explosion. An adaptive law is proposed to estimate the upper boundaries of uncertainties. Lyapunov function is used to prove the stability of the closed-loop system. Finally, numerical simulation results indicate the effectiveness of the designed control method.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"14 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114230726","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2021-10-01DOI: 10.1109/icmeas54189.2021.00016
R. Du, Xing Zhang, Xiang Zhang, Ling Wang, W. Liao
It has been anticipated that CubeSats would have wide applications in on-orbit servicing (OOS) fields due to their advantages of short research and development cycle and low manufacturing cost, in which the close-range relative navigation is a critical technique that usually requires high accuracy of the relative pose estimation. This paper proposes a vision-based relative navigation sensor for OOS of CubeSats. A set of active fiducial markers with multi-layer structure was designed to ensure an accurate unambiguous matching and measurement. An improved effective perspective-n-point (IEPnP) algorithm is developed to obtain an accurate relative state estimation. An experiment system which simulates the real illumination and motion conditions in space was set up to assess the performances of the proposed sensor. The results show that the sensor can overcome the interference of the ambient light, and can reach an accuracy of range estimation smaller than 2 mm and an accuracy of relative attitude estimation smaller than 0.4 deg at distance of 1 m. Through contrast tests, the accuracy of the proposed IEPnP algorithm is better than the classical perspective-3-point (P3P) algorithm and EPnP algorithm.
{"title":"A vision-based relative navigation sensor for on-orbit servicing of CubeSats","authors":"R. Du, Xing Zhang, Xiang Zhang, Ling Wang, W. Liao","doi":"10.1109/icmeas54189.2021.00016","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00016","url":null,"abstract":"It has been anticipated that CubeSats would have wide applications in on-orbit servicing (OOS) fields due to their advantages of short research and development cycle and low manufacturing cost, in which the close-range relative navigation is a critical technique that usually requires high accuracy of the relative pose estimation. This paper proposes a vision-based relative navigation sensor for OOS of CubeSats. A set of active fiducial markers with multi-layer structure was designed to ensure an accurate unambiguous matching and measurement. An improved effective perspective-n-point (IEPnP) algorithm is developed to obtain an accurate relative state estimation. An experiment system which simulates the real illumination and motion conditions in space was set up to assess the performances of the proposed sensor. The results show that the sensor can overcome the interference of the ambient light, and can reach an accuracy of range estimation smaller than 2 mm and an accuracy of relative attitude estimation smaller than 0.4 deg at distance of 1 m. Through contrast tests, the accuracy of the proposed IEPnP algorithm is better than the classical perspective-3-point (P3P) algorithm and EPnP algorithm.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"156 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132549201","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2021-10-01DOI: 10.1109/icmeas54189.2021.00028
Liyong Huang, Shaolin Chen, Zhihui Wang
Turbocharged is very important for engine emission reduction of road vehicles. The performance of turbocharged engine was strongly affected by heat transfer of turbocharger. The aim of this studyis to evaluate the effect of turbocharger cooling and lubricating state on the performance of turbocharged engine. This work was developed a detailed model that evaluating both engine performance and turbocharger cooling and lubricating state. The simulated model was validated by the experimental data on the turbocharger and engine test bench. Finally, this model has been used to evaluate the engine performance under three different heat transfer conditions. The results showing the mass flow rate of turbocharger cooling water is an important factor for turbocharged engine performance, especially for the temperature of engine exhaust emission.
{"title":"Impact of turbocharger cooling and lubricating state on the Performance of Turbocharged Engine","authors":"Liyong Huang, Shaolin Chen, Zhihui Wang","doi":"10.1109/icmeas54189.2021.00028","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00028","url":null,"abstract":"Turbocharged is very important for engine emission reduction of road vehicles. The performance of turbocharged engine was strongly affected by heat transfer of turbocharger. The aim of this studyis to evaluate the effect of turbocharger cooling and lubricating state on the performance of turbocharged engine. This work was developed a detailed model that evaluating both engine performance and turbocharger cooling and lubricating state. The simulated model was validated by the experimental data on the turbocharger and engine test bench. Finally, this model has been used to evaluate the engine performance under three different heat transfer conditions. The results showing the mass flow rate of turbocharger cooling water is an important factor for turbocharged engine performance, especially for the temperature of engine exhaust emission.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"12 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130431224","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2021-10-01DOI: 10.1109/icmeas54189.2021.00021
D. Nagy
This paper exemplifies the influence of the purpose of an aircraft on the aerodynamic properties of its airfoil. In particular, the research takes into consideration two types of aircraft, namely cargo aircraft and military high-speed aircraft and compares their airfoil characteristics using their NACA airfoils as well as computational fluid dynamics. The results show that airfoils of aircraft designed for cargo have a heavier focus on maintaining a large lift force whereas speedoriented airplanes focus on minimizing the drag force.
{"title":"Simulations of NACA 65-415 and NACA 64-206 Airfoils using Computational Fluid Dynamics","authors":"D. Nagy","doi":"10.1109/icmeas54189.2021.00021","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00021","url":null,"abstract":"This paper exemplifies the influence of the purpose of an aircraft on the aerodynamic properties of its airfoil. In particular, the research takes into consideration two types of aircraft, namely cargo aircraft and military high-speed aircraft and compares their airfoil characteristics using their NACA airfoils as well as computational fluid dynamics. The results show that airfoils of aircraft designed for cargo have a heavier focus on maintaining a large lift force whereas speedoriented airplanes focus on minimizing the drag force.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"17 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133391560","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
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