2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)最新文献

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Research on Geometry Configuration/Fuel Distribution of Combustion Chamber of Scramjet 超燃冲压发动机燃烧室几何构型及燃料分布研究
2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE) Pub Date : 2018-07-01 DOI: 10.1109/ICMAE.2018.8467713
Hao-min Li, Yu-chun Chen, Chun Guan, Yuan Gao, Zhi-hua Wang, Yu-sang Li
{"title":"Research on Geometry Configuration/Fuel Distribution of Combustion Chamber of Scramjet","authors":"Hao-min Li, Yu-chun Chen, Chun Guan, Yuan Gao, Zhi-hua Wang, Yu-sang Li","doi":"10.1109/ICMAE.2018.8467713","DOIUrl":"https://doi.org/10.1109/ICMAE.2018.8467713","url":null,"abstract":"In this article, based on the reference configuration of combustion chamber of scramjet, the influence of design point parameters of the two-stage combustion chamber geometry configuration and fuel distribution ratio on engine performance is studied, and thrust and specific impulse are used as the overall performance evaluation parameters, the comparison and evaluation of the mobility and economy of the engine provide certain references for the selection of design point parameters of the combustion chamber geometry configuration and fuel distribution ratio. The results show that increasing the area of the thermal throat of the combustion chamber by increasing the two-stage expansion ratio of the combustion chamber can increase the thrust at low speed and enhance the mobility of the aircraft; when it does not cause thermal choke and does not affect the start-up of the inlet, increasing the fuel distribution ratio in the first stage of the combustion chamber can increase the engine’s specific impulse, thereby improve the economy of the aircraft.","PeriodicalId":118501,"journal":{"name":"2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121786810","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}
引用次数: 2
Nonhomogeneous Boundary Value Problem for a Semi-strip Clamped at the End: Exact Solution 端部夹紧半带材的非齐次边值问题:精确解
2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE) Pub Date : 2018-07-01 DOI: 10.1109/ICMAE.2018.8467674
A. P. Kerzhaev
{"title":"Nonhomogeneous Boundary Value Problem for a Semi-strip Clamped at the End: Exact Solution","authors":"A. P. Kerzhaev","doi":"10.1109/ICMAE.2018.8467674","DOIUrl":"https://doi.org/10.1109/ICMAE.2018.8467674","url":null,"abstract":"In the paper, on the basis of the solution of the biharmonic problem for a smooth semi-strip and the method of the integral Fourier transform, is constructed the exact solution of a nonhomogeneous boundary value problem for a semi-strip clamped at the end (a concentrated force is applied inside the domain along the horizontal axis). The solution is constructed on the superposition principle in the form of the sum of integrals and series in trigonometric functions and Papkovich–Fadle eigenfunctions. The coefficients of these expansions are determined by simple formulas as the Fourier integrals of given boundary functions.","PeriodicalId":118501,"journal":{"name":"2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"164 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132346916","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}
引用次数: 0
ICMAE 2018 Copyright Page ICMAE 2018版权页面
2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE) Pub Date : 2018-07-01 DOI: 10.1109/icmae.2018.8467676
{"title":"ICMAE 2018 Copyright Page","authors":"","doi":"10.1109/icmae.2018.8467676","DOIUrl":"https://doi.org/10.1109/icmae.2018.8467676","url":null,"abstract":"","PeriodicalId":118501,"journal":{"name":"2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"78 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114534487","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}
引用次数: 0
A Method of Carrier Landing Position Prediction Based on Sinusoidal Model 一种基于正弦模型的航母着陆位置预测方法
2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE) Pub Date : 2018-07-01 DOI: 10.1109/ICMAE.2018.8467615
Jianzhi Wang, Gang Liu, Guanxin Hong
{"title":"A Method of Carrier Landing Position Prediction Based on Sinusoidal Model","authors":"Jianzhi Wang, Gang Liu, Guanxin Hong","doi":"10.1109/ICMAE.2018.8467615","DOIUrl":"https://doi.org/10.1109/ICMAE.2018.8467615","url":null,"abstract":"The safety of the aircraft landing is one of the important factors limiting the combat capability of an aircraft carrier. It is difficult for the carrier-based aircraft to land because of random movements of aircraft carriers in the ocean. In this paper, a method to predict the position of aircraft carrier based on ship motion model is studied. The simulation shows that, except for the extreme special cases, the theil inequality coefficient (TIC) of the predicted data and the reference data can be less than 0.3 which means forecasts are acceptable. This method is simple in calculation, quick in response, and does not rely on a large amount of historical data and complex preparatory work. The approach has advantages in the context of dramatic environmental changes and the carrier landing of small unmanned aircraft.","PeriodicalId":118501,"journal":{"name":"2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"75 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134513571","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}
引用次数: 1
A Study of Close-Formation Approach Attack Tactics of Multiple Anti-Ship Missiles 多反舰导弹近编队进场攻击战术研究
2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE) Pub Date : 2018-07-01 DOI: 10.1109/ICMAE.2018.8467681
Y. An, Kuk-Kwon Park, C. Ryoo
{"title":"A Study of Close-Formation Approach Attack Tactics of Multiple Anti-Ship Missiles","authors":"Y. An, Kuk-Kwon Park, C. Ryoo","doi":"10.1109/ICMAE.2018.8467681","DOIUrl":"https://doi.org/10.1109/ICMAE.2018.8467681","url":null,"abstract":"In this paper, we suggested a ‘Close-Formation Approach’ attack tactics as a new tactics to operate multiple anti-ship missiles. This tactics is suggested to increase the survivability of anti-ship missiles in multi-layered ship defense system, and the close-formation flight of the missiles makes it possible to neutralize the ship defense system by deceiving the radar of the ship. We modeled the scattering points, which are the radar measurements, and analyzed the close-formation flight characteristics of two missiles. The ‘identification range’ is calculated through the analysis. It is the relative range from the ship when two missiles are started to distinguish each other. Based on this, we implemented the suggested tactics and analyzed the effectiveness through Monte-Carlo simulation.","PeriodicalId":118501,"journal":{"name":"2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"55 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131561752","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}
引用次数: 0
An Overview of Gamma Prime Precipitates Rafting in Ni-Based SC Superalloys: Degradation Kinetics, Modeling and Relations with Mechanical Properties ni基SC高温合金中γ素体沉淀:降解动力学、建模及其与力学性能的关系
2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE) Pub Date : 2018-07-01 DOI: 10.1109/ICMAE.2018.8467647
Hanzhi Chen
{"title":"An Overview of Gamma Prime Precipitates Rafting in Ni-Based SC Superalloys: Degradation Kinetics, Modeling and Relations with Mechanical Properties","authors":"Hanzhi Chen","doi":"10.1109/ICMAE.2018.8467647","DOIUrl":"https://doi.org/10.1109/ICMAE.2018.8467647","url":null,"abstract":"Single crystal (SC) Ni-based superalloys are widely used as the crucial components manufacturing in the turbine blades and land-based gas turbines due to their high tensile strength, stability, and thermal efficiency etc. Microstructure degradation such as rafting, is an essential phenomenon that affects the mechanical properties of the materials in severe service environment to some extent. Hence, it is significant to understand the kinetics of rafting. Besides, quantitative analysis methodology of degradation kinetics investigation is also important. In present overview, specific differences of coarsening and rafting are illustrated in clear comparisons and reviewed to reduce ambiguity in the research works. Subsequently, a new technique which can effectively enhance the experimental efficiency during Ni-based superalloys investigation is introduced. Two classical degradation models to analyze the rafting kinetics are additionally evaluated and compared. Finally, the influence of rafting on the mechanical properties and recent experimental results related are discussed.","PeriodicalId":118501,"journal":{"name":"2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"7 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133273442","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}
引用次数: 1
Analysis for UAV Heuristic Tracking Path Planning Based on Target Matching 基于目标匹配的无人机启发式跟踪路径规划分析
2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE) Pub Date : 2018-07-01 DOI: 10.1109/ICMAE.2018.8467659
Changwu Zhang, Hengzhu Liu, Yuchen Tang
{"title":"Analysis for UAV Heuristic Tracking Path Planning Based on Target Matching","authors":"Changwu Zhang, Hengzhu Liu, Yuchen Tang","doi":"10.1109/ICMAE.2018.8467659","DOIUrl":"https://doi.org/10.1109/ICMAE.2018.8467659","url":null,"abstract":"Target tracking is a hot research direction in the UAV path planning, and there are many related researches, especially for the design of algorithms. In this paper, the heuristic tracking path planning is studied from the aspects of target matching, algorithm design and parameters analysis, realizing the autonomous processing ability of UAV from target selection to path planning, and the influence of each parameter on the path planning result was emphatically analyzed. In the process of target matching, the Hungarian algorithm was used to solve the problem. During the path planning process, the target tracking A* algorithm was designed. The parameters analysis mainly includes the step size, turning angle, the proportion of the heuristic function and the number of threats in the flight node expansion process. The simulation result of tracking path planning is given in the article, which shows the feasibility of this method.","PeriodicalId":118501,"journal":{"name":"2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"27 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133708217","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}
引用次数: 3
Elasto-Plastic Stress Analysis Methodology Establishment for Forging Dies 锻模弹塑性应力分析方法的建立
2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE) Pub Date : 2018-07-01 DOI: 10.1109/ICMAE.2018.8467701
Dattaprasad Lomate, Govind Jagtap, Mr. Abhijit Patil, Mr. Sanket Inamdar, D. R. Singh, Manoj Ukhande
{"title":"Elasto-Plastic Stress Analysis Methodology Establishment for Forging Dies","authors":"Dattaprasad Lomate, Govind Jagtap, Mr. Abhijit Patil, Mr. Sanket Inamdar, D. R. Singh, Manoj Ukhande","doi":"10.1109/ICMAE.2018.8467701","DOIUrl":"https://doi.org/10.1109/ICMAE.2018.8467701","url":null,"abstract":"Finite Element Analysis (FEA) is an important engineering tool used to assist in approximating and verifying how a component will react under various complex loading conditions. There are many conditions where the stress applied could extend beyond the yield point of the material but FEA does not necessarily provide visual indication that the part has yielded. Elastic material property has a linear stress-strain relationship regardless of the load applied while the elastic-plastic has a linear relationship up to yield point and then becomes nonlinear beyond yield point.In this study tensile tests and finite element analysis were carried out on forging die material. The unidirectional monotonic tensile tests were carried out on MTS machine. The Hypermesh and ANSYS FEA tools are used for elastic and elastic-plastic FEA. The mechanical behavior and stresses at critical locations under realistic forging process loading condition is investigated based on elastic and elastic-plastic FEA. Specifically, the elastic-plastic response under forging loading conditions beyond the elastic limit is studied. The stress - strain of die material was determined and used as input of a nonlinear finite element study aimed at investigating the stress evolution in the forging die. The forging die elastic FEA was carried out based on basic material properties, while elastic-plastic FEA was carried out based on material nonlinearity Von misses isotropic hardening plasticity criteria. The study concludes that elastic- plastic FEA gives more accurate die stress value and critical locations.","PeriodicalId":118501,"journal":{"name":"2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"575 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116260729","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}
引用次数: 0
An Adaptive Feedback Turning SIR Particle Filter and Its Application on Fault Diagnosis of Auxiliary Power Unit 自适应反馈旋转SIR粒子滤波及其在辅助动力机组故障诊断中的应用
2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE) Pub Date : 2018-07-01 DOI: 10.1109/ICMAE.2018.8467610
Kai Peng, Yingjie Hu, D. Fan, Fan Yang, Zhaorong Zhang
{"title":"An Adaptive Feedback Turning SIR Particle Filter and Its Application on Fault Diagnosis of Auxiliary Power Unit","authors":"Kai Peng, Yingjie Hu, D. Fan, Fan Yang, Zhaorong Zhang","doi":"10.1109/ICMAE.2018.8467610","DOIUrl":"https://doi.org/10.1109/ICMAE.2018.8467610","url":null,"abstract":"With the development of aero-engine control technology, the complexity of the control system is getting higher and higher, and the requirements of high security and reliability have made fault diagnosis more urgent. Because of the bad working environment, the sensor is very prone to malfunction. Because SIR particle filter can be used to implement the estimation of the engine state parameters in the fault diagnosis of the sensor and is inefficient and inaccuracy in state estimation, an adaptive feedback correction mechanism is provided to improve particle degradation in SIR particle filter in the estimation. The simulations show that the proposed method improves the estimation precision of exhaust temperature of Auxiliary Power Unit (APU) during bias failure, drift failure, and power failure of temperature sensor.","PeriodicalId":118501,"journal":{"name":"2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"24 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123709250","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}
引用次数: 1
Design of Repetitive Controller Using Optimization in Frequency Domain with Maximum Gain Constraints 基于最大增益约束的频域优化重复控制器设计
2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE) Pub Date : 2018-07-01 DOI: 10.1109/ICMAE.2018.8467704
Pitcha Prasitmeeboon
{"title":"Design of Repetitive Controller Using Optimization in Frequency Domain with Maximum Gain Constraints","authors":"Pitcha Prasitmeeboon","doi":"10.1109/ICMAE.2018.8467704","DOIUrl":"https://doi.org/10.1109/ICMAE.2018.8467704","url":null,"abstract":"Spacecraft inherently have rotating parts such as the momentum wheels, reaction wheels or CMGs. Slight imbalances can produce vibrations that disturb fine pointing equipment. Repetitive control (RC) can be applied on an active vibration isolation to eliminate the effect of such periodic disturbances. An effective RC design method based on optimization in frequency domain was presented. In situations that a system needs large amount of correction, a compensator with high gains can generate a command that exceeds the capacity of the equipment. The error continues to grow and the system will become unstable. A method to reduce the magnitude of the compensator gains available in literature requires a weighting function that is difficult to design. This paper presents an alternative method to design an RC compensator that can limit the maximum magnitude of compensator gains. Simulation results show that the proposed method is more effective than the existing method.","PeriodicalId":118501,"journal":{"name":"2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"54 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126608787","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}
引用次数: 1
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