Pub Date : 2016-07-18DOI: 10.1109/ICMAE.2016.7549507
C. Kannan, R. Ramesh, Rishi S. Vaidya, B. Vijayaram
Suppression of vibration is one of the functional requirement in structures subjected to dynamic conditions like machine tools, automobile parts etc. To impart increased dynamic stiffness and strength to woven fabric carbon epoxy composite structures, micro rubber particles of average size 5μm and 20nm nano silica particles were added and its dynamic response was evaluated by experimental forced vibration study. The carbon epoxy composite beams were compared with carbon composite containing 9 wt. % of micro rubber particles and 11wt. % of nano silica particles. Carbon epoxy beams were fabricated by hand layup method by considering Box and Channel cross sectional shape. A fiber volume fraction of 40% and a matrix volume fraction of 60% were preferred as a composition for all considered beams. Six-layered carbon/epoxy beam with uniform cross-sectional area, height to width ratio, and moment of inertia were considered. Forcing sine wave motion was given to the composite beams through higher order stinger which is connecting between free end of the beam and electrodynamic shaker. The forced vibration test was conducted for the frequency range from 50 to 80 Hz with two different forcing amplitudes of 0.05 mm and 0.1mm. The responses show the variation in dynamic performance of carbon when compared with dedicated carbon beam. Closed cross sectional box shape shows improved performance than open channel shaped beam under forced vibration condition.
{"title":"Investigation on forced vibration response of micro rubber/nano silica added carbon composite beams for structural applications","authors":"C. Kannan, R. Ramesh, Rishi S. Vaidya, B. Vijayaram","doi":"10.1109/ICMAE.2016.7549507","DOIUrl":"https://doi.org/10.1109/ICMAE.2016.7549507","url":null,"abstract":"Suppression of vibration is one of the functional requirement in structures subjected to dynamic conditions like machine tools, automobile parts etc. To impart increased dynamic stiffness and strength to woven fabric carbon epoxy composite structures, micro rubber particles of average size 5μm and 20nm nano silica particles were added and its dynamic response was evaluated by experimental forced vibration study. The carbon epoxy composite beams were compared with carbon composite containing 9 wt. % of micro rubber particles and 11wt. % of nano silica particles. Carbon epoxy beams were fabricated by hand layup method by considering Box and Channel cross sectional shape. A fiber volume fraction of 40% and a matrix volume fraction of 60% were preferred as a composition for all considered beams. Six-layered carbon/epoxy beam with uniform cross-sectional area, height to width ratio, and moment of inertia were considered. Forcing sine wave motion was given to the composite beams through higher order stinger which is connecting between free end of the beam and electrodynamic shaker. The forced vibration test was conducted for the frequency range from 50 to 80 Hz with two different forcing amplitudes of 0.05 mm and 0.1mm. The responses show the variation in dynamic performance of carbon when compared with dedicated carbon beam. Closed cross sectional box shape shows improved performance than open channel shaped beam under forced vibration condition.","PeriodicalId":371629,"journal":{"name":"2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"6 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133984481","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 : 2016-07-18DOI: 10.1109/ICMAE.2016.7549519
P. Martínek, P. Podaný, M. Koukolíková, J. Dlouhý, M. Duchek
This paper deals with heat treatment of a manganese TRIP/TWIP steel containing various aluminium levels. Two heats were made with identical chemical compositions, apart from different aluminium levels: 0.4 and 1.4 wt. %. Cold-rolled sheets were made using a route in which the last forming operation involved 40 % reduction, and then annealed. The annealing times were 1, 2, and 3 hours. On the specimens taken from the annealed sheets, microstructures were examined and grain size, phase fractions and hardness were measured. These results were compared between the two heats to identity the impact of the aluminium level on properties of this steel. In addition, the results were compared with the data for the initial condition of the materials.
{"title":"Properties of TRIP/TWIP steel with different aluminium levels upon annealing","authors":"P. Martínek, P. Podaný, M. Koukolíková, J. Dlouhý, M. Duchek","doi":"10.1109/ICMAE.2016.7549519","DOIUrl":"https://doi.org/10.1109/ICMAE.2016.7549519","url":null,"abstract":"This paper deals with heat treatment of a manganese TRIP/TWIP steel containing various aluminium levels. Two heats were made with identical chemical compositions, apart from different aluminium levels: 0.4 and 1.4 wt. %. Cold-rolled sheets were made using a route in which the last forming operation involved 40 % reduction, and then annealed. The annealing times were 1, 2, and 3 hours. On the specimens taken from the annealed sheets, microstructures were examined and grain size, phase fractions and hardness were measured. These results were compared between the two heats to identity the impact of the aluminium level on properties of this steel. In addition, the results were compared with the data for the initial condition of the materials.","PeriodicalId":371629,"journal":{"name":"2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"44 5","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133390596","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 : 2016-07-18DOI: 10.1109/ICMAE.2016.7549559
Hongkang Liu, Chao Yan, Yatian Zhao, Bo-xi Lin
Load balancing is one of the critical factors affecting the performance of parallel computing. An improved partitioning strategy is proposed for structured multiblock grids here. The new subgrid-splitting approach, together with a recursive graph-partitioning algorithm, is to seek a good load balancing as less blocks as possible. Two typical applications are implemented to validate the strategy. Results demonstrate that the new partitioning strategy behaves well in load balancing and communication overheads, and furthermore manifests an excellent performance in decreasing the amount of blocks, as well as the memory requirement caused by the multiplication of ghost cells near the edge.
{"title":"An improved partitioning strategy for structured multiblock grids","authors":"Hongkang Liu, Chao Yan, Yatian Zhao, Bo-xi Lin","doi":"10.1109/ICMAE.2016.7549559","DOIUrl":"https://doi.org/10.1109/ICMAE.2016.7549559","url":null,"abstract":"Load balancing is one of the critical factors affecting the performance of parallel computing. An improved partitioning strategy is proposed for structured multiblock grids here. The new subgrid-splitting approach, together with a recursive graph-partitioning algorithm, is to seek a good load balancing as less blocks as possible. Two typical applications are implemented to validate the strategy. Results demonstrate that the new partitioning strategy behaves well in load balancing and communication overheads, and furthermore manifests an excellent performance in decreasing the amount of blocks, as well as the memory requirement caused by the multiplication of ghost cells near the edge.","PeriodicalId":371629,"journal":{"name":"2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"49 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133789296","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 : 2016-07-18DOI: 10.1109/ICMAE.2016.7549525
C. Mahesh, A. Valavade
In the present work, ventilated disc brake rotors with variable diameter circular pillar configurations were analyzed to enhance the heat dissipation and obtain more uniform temperature distribution in the rotor. CFD code used in this work was validated with experimental results obtained by conducting experiments on a test rig. Experimental analysis was performed on existing taper radial vane (TRV) rotor to calculate the mass flow rate and heat transfer coefficient. Further, variable diameter circular pillar (VDCP) rotor with different configurations namely VDCP1, VDCP2 and VDCP3 were considered for the analysis. A 20° segment of rotor was considered for the numerical analysis due to its rotational symmetry. CFD results were in good agreement with the experimental analysis. The maximum deviation of numerical results were about 15% from the experimental results. It is found from the analysis that among all the rotor configurations; VDCP1 rotor configuration gives better rate of heat dissipation and more uniform temperature distribution in the rotor. Hence for modern high speed vehicles VDCP1 rotor configuration may be more appropriate.
{"title":"Flow and heat transfer analysis of variable diameter circular pillar disc brake rotor using CFD","authors":"C. Mahesh, A. Valavade","doi":"10.1109/ICMAE.2016.7549525","DOIUrl":"https://doi.org/10.1109/ICMAE.2016.7549525","url":null,"abstract":"In the present work, ventilated disc brake rotors with variable diameter circular pillar configurations were analyzed to enhance the heat dissipation and obtain more uniform temperature distribution in the rotor. CFD code used in this work was validated with experimental results obtained by conducting experiments on a test rig. Experimental analysis was performed on existing taper radial vane (TRV) rotor to calculate the mass flow rate and heat transfer coefficient. Further, variable diameter circular pillar (VDCP) rotor with different configurations namely VDCP1, VDCP2 and VDCP3 were considered for the analysis. A 20° segment of rotor was considered for the numerical analysis due to its rotational symmetry. CFD results were in good agreement with the experimental analysis. The maximum deviation of numerical results were about 15% from the experimental results. It is found from the analysis that among all the rotor configurations; VDCP1 rotor configuration gives better rate of heat dissipation and more uniform temperature distribution in the rotor. Hence for modern high speed vehicles VDCP1 rotor configuration may be more appropriate.","PeriodicalId":371629,"journal":{"name":"2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"13 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124497292","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 : 2016-07-18DOI: 10.1109/ICMAE.2016.7549510
H. Dalir
The design of aircraft composite stiffened structures subjected to dynamic and impact loadings requires several experimental testing scenarios on the full-size structure. The present paper deals with investigating the feasibility of the use of sub-size test specimens under vertical and lateral impacts on the stiffener free flange based on finite element (FE) models. Simulations were performed on sub-size specimens carefully extracted from the full-size (26.4 × 48.4 × 2.4 in3) impact test panels. The main required specifications of an in-house falling weight impact tester were also determined, discussing the required fixture/jig configuration.
{"title":"Damage tolerance coupon sizing of composite stiffened panels under impact","authors":"H. Dalir","doi":"10.1109/ICMAE.2016.7549510","DOIUrl":"https://doi.org/10.1109/ICMAE.2016.7549510","url":null,"abstract":"The design of aircraft composite stiffened structures subjected to dynamic and impact loadings requires several experimental testing scenarios on the full-size structure. The present paper deals with investigating the feasibility of the use of sub-size test specimens under vertical and lateral impacts on the stiffener free flange based on finite element (FE) models. Simulations were performed on sub-size specimens carefully extracted from the full-size (26.4 × 48.4 × 2.4 in3) impact test panels. The main required specifications of an in-house falling weight impact tester were also determined, discussing the required fixture/jig configuration.","PeriodicalId":371629,"journal":{"name":"2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"20 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116868590","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 : 2016-07-18DOI: 10.1109/ICMAE.2016.7549574
Tang Changliang, Yang Jinfu, Han Dongjiang, Lei Huan
The flywheel energy storage technology is a new type of conversion and storage for electric energy, and it is also a research hotspot of energy field in the world. There are a large number of studies on dynamic characteristics of energy storage flywheel in recent years. The flexible support with a single point has small load-carrying ability but very low friction loss, which is appropriate to be used in small flywheel system. For this reason, a flywheel shafting with a single point flexible support was established. By means of the Lagrangian equation, the special dynamic model of the flywheel rotor-bearing-damper was built to calculate critical speed, modal shape and modal damping ratio with different speed. The results show that shafting is stable, simple and efficient. And the experimental result is in agreement with the theoretical one.
{"title":"Rotor dynamics analysis and experimental research of flywheel shafting with a single point flexible support","authors":"Tang Changliang, Yang Jinfu, Han Dongjiang, Lei Huan","doi":"10.1109/ICMAE.2016.7549574","DOIUrl":"https://doi.org/10.1109/ICMAE.2016.7549574","url":null,"abstract":"The flywheel energy storage technology is a new type of conversion and storage for electric energy, and it is also a research hotspot of energy field in the world. There are a large number of studies on dynamic characteristics of energy storage flywheel in recent years. The flexible support with a single point has small load-carrying ability but very low friction loss, which is appropriate to be used in small flywheel system. For this reason, a flywheel shafting with a single point flexible support was established. By means of the Lagrangian equation, the special dynamic model of the flywheel rotor-bearing-damper was built to calculate critical speed, modal shape and modal damping ratio with different speed. The results show that shafting is stable, simple and efficient. And the experimental result is in agreement with the theoretical one.","PeriodicalId":371629,"journal":{"name":"2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123618496","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 : 2016-07-18DOI: 10.1109/ICMAE.2016.7549532
H. Rezaiguia, Peijin Liu
The experimental work presented in this paper deals with the flame response of a solid laminate propellant AP/HTPB to pressure perturbations. Experiments were performed in closed tube pressurized under 1MPa. The pressure perturbations are created by a pulser system connected to the end of the combustion chamber. The combustion process of a three layers of AP/HTPB was recorded by using a microscope and a high speed camera. The qualitative analysis of the flame images of the two cases, with and without pressure fluctuations, revealed that the standing acoustic waves established in the tube has strongly affected the flame and the combustion products flow. The flame response was translated by an oscillation motion above the burning surface. Thus, the burning surface profile was changed which means that the regression rate value may fluctuate.
{"title":"Flame response of solid laminate propellant AP/HTPB to pressure perturbations","authors":"H. Rezaiguia, Peijin Liu","doi":"10.1109/ICMAE.2016.7549532","DOIUrl":"https://doi.org/10.1109/ICMAE.2016.7549532","url":null,"abstract":"The experimental work presented in this paper deals with the flame response of a solid laminate propellant AP/HTPB to pressure perturbations. Experiments were performed in closed tube pressurized under 1MPa. The pressure perturbations are created by a pulser system connected to the end of the combustion chamber. The combustion process of a three layers of AP/HTPB was recorded by using a microscope and a high speed camera. The qualitative analysis of the flame images of the two cases, with and without pressure fluctuations, revealed that the standing acoustic waves established in the tube has strongly affected the flame and the combustion products flow. The flame response was translated by an oscillation motion above the burning surface. Thus, the burning surface profile was changed which means that the regression rate value may fluctuate.","PeriodicalId":371629,"journal":{"name":"2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"42 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125022386","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 : 2016-07-18DOI: 10.1109/ICMAE.2016.7549547
Jianbin Zou, K. Gao, Jie Yang, Jiang Zhu
For the weakness of passive radar seeker (PRS), anti-radiation weapons (ARW) could be jammed easily by two decoys with same frequency. Compared with the high complexity of actualization of traditional angle differentiation methods, a method based on Doppler frequency difference (DFD) of received decoys' signals is presented to distinguish jamming decoy sources with the same frequencies, which has low complexity and easily be actualized. Factors that affect DFD are analyzed in detail. Then differentiation region of PRS telling decoys apart is analysed. The simulation results prove that this method can improve the ability of anti-radiation weapon confronting active decoys effectively.
{"title":"Research on anti-radiation weapon confronting active decoys based on Doppler frequencies difference","authors":"Jianbin Zou, K. Gao, Jie Yang, Jiang Zhu","doi":"10.1109/ICMAE.2016.7549547","DOIUrl":"https://doi.org/10.1109/ICMAE.2016.7549547","url":null,"abstract":"For the weakness of passive radar seeker (PRS), anti-radiation weapons (ARW) could be jammed easily by two decoys with same frequency. Compared with the high complexity of actualization of traditional angle differentiation methods, a method based on Doppler frequency difference (DFD) of received decoys' signals is presented to distinguish jamming decoy sources with the same frequencies, which has low complexity and easily be actualized. Factors that affect DFD are analyzed in detail. Then differentiation region of PRS telling decoys apart is analysed. The simulation results prove that this method can improve the ability of anti-radiation weapon confronting active decoys effectively.","PeriodicalId":371629,"journal":{"name":"2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"40 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127161879","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 : 2016-07-18DOI: 10.1109/ICMAE.2016.7549614
Kun Fang, R. Xue, Yanbo Zhu
To eliminate the time correlation and model the heavy distribution tail of ground based augmentation system (GBAS) errors, a method utilizing generalized autoregressive conditional heteroscedasticity (GARCH) model is introduced in this paper. Considering the statistical uncertainty of model parameters, a strategy for using the GARCH model in nonstationary situations is proposed. Based on that, a protection level calculation framework is established with an online/offline structure to calculate error overbound and protection level in real time. As the heavy-tail errors are normalized to standard Gaussian distribution, and all the normalized errors from different satellites and elevation groups are mixed together to calculate Gaussian overbound, the Gaussian overbound is much tighter than the one calculated by classic heavy-tail errors. That leads to smaller protection levels and higher system availability.
{"title":"GBAS protection level calculation with GARCH model","authors":"Kun Fang, R. Xue, Yanbo Zhu","doi":"10.1109/ICMAE.2016.7549614","DOIUrl":"https://doi.org/10.1109/ICMAE.2016.7549614","url":null,"abstract":"To eliminate the time correlation and model the heavy distribution tail of ground based augmentation system (GBAS) errors, a method utilizing generalized autoregressive conditional heteroscedasticity (GARCH) model is introduced in this paper. Considering the statistical uncertainty of model parameters, a strategy for using the GARCH model in nonstationary situations is proposed. Based on that, a protection level calculation framework is established with an online/offline structure to calculate error overbound and protection level in real time. As the heavy-tail errors are normalized to standard Gaussian distribution, and all the normalized errors from different satellites and elevation groups are mixed together to calculate Gaussian overbound, the Gaussian overbound is much tighter than the one calculated by classic heavy-tail errors. That leads to smaller protection levels and higher system availability.","PeriodicalId":371629,"journal":{"name":"2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"33 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129063100","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 : 2016-07-18DOI: 10.1109/ICMAE.2016.7549546
Min Wang, Yunan Liu, Tao Zan, Xiang-sheng Gao, Yanlin Zhang
Residual stress of thin-walled blanks with complex cavity structure is an important influence factor on the stability of machining. The most residual stress testing technologies is only suitable to measure residual stress of surface or shallow surface. It is difficult to ensure the accuracy to measure residual stress inside workpiece. In order to study the reliability and accuracy of incremental hole drilling method measuring interior residual stress, according to residual stress test for casting ZL205A aluminum alloy tapered thin-walled blank, finite element (FE) model with initial residual stress is established to simulate incremental hole drilling on the platform of ANSYS. Then error and the rationality of the finite element simulation model has been analyzed by comparing the simulation stress value with the test. The results indicate that the incremental hole drilling method has some errors to measures residual stress inside workpiece. The method is only suitable to measure surface residual stress.
{"title":"Residual stress test and simulation of incremental hole drilling method","authors":"Min Wang, Yunan Liu, Tao Zan, Xiang-sheng Gao, Yanlin Zhang","doi":"10.1109/ICMAE.2016.7549546","DOIUrl":"https://doi.org/10.1109/ICMAE.2016.7549546","url":null,"abstract":"Residual stress of thin-walled blanks with complex cavity structure is an important influence factor on the stability of machining. The most residual stress testing technologies is only suitable to measure residual stress of surface or shallow surface. It is difficult to ensure the accuracy to measure residual stress inside workpiece. In order to study the reliability and accuracy of incremental hole drilling method measuring interior residual stress, according to residual stress test for casting ZL205A aluminum alloy tapered thin-walled blank, finite element (FE) model with initial residual stress is established to simulate incremental hole drilling on the platform of ANSYS. Then error and the rationality of the finite element simulation model has been analyzed by comparing the simulation stress value with the test. The results indicate that the incremental hole drilling method has some errors to measures residual stress inside workpiece. The method is only suitable to measure surface residual stress.","PeriodicalId":371629,"journal":{"name":"2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE)","volume":"32 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130769945","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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