Pub Date : 2013-05-02DOI: 10.1109/IBCAST.2013.6512125
T. Rasheed, S. Akbar, S. Mirza
This paper presents method for the characterization of composite tubes produced by filament winding technique. The aim of this study is to investigate the mechanical properties by tensile test and under internal pressure loads. For this purpose specimens produced with different orientation having the same reinforcement with two different matrix systems. Data produced experimentally by measuring the mechanical properties like longitudinal tensile and hoop tensile properties, strain in hoop direction and maximum hoop stresses during the hydraulic testing. In order to investigate these parameters, internal pressure tests are done on the filament-wound composite tubes having internal diameter 64.5± 0.5 mm and length 320± 2.0 mm according to ASTM D 1599-99 standard. The tubes for the testing are manufactured by wet filament winding methods of [± 60°] E-glass/Epoxy of various wall thicknesses. Hydraulic tests revealed that the tubes with winding orientation [± 60°]2[±90°]2 exhibits better burst performance compared with others orientations. In addition, factors affecting the behavior of the tubes like buckling, stress variation through wall thickness are discussed.
本文介绍了长丝缠绕复合材料管的表征方法。本研究的目的是通过拉伸试验和内压载荷来研究其力学性能。为此，用两种不同的基体体系制作具有不同取向、相同配筋的试样。通过测量水力测试期间的纵向拉伸和环向拉伸性能、环向应变和最大环向应力等力学性能的实验数据。根据ASTM D 1599-99标准，对内径64.5±0.5 mm、长度320±2.0 mm的丝绕复合材料管进行了内压试验。用于测试的管是用不同壁厚的[±60°]e -玻璃/环氧树脂湿长丝缠绕法制造的。水力试验结果表明，缠绕方向为[±60°]2[±90°]2的管具有较好的爆破性能。此外，还讨论了影响管的屈曲、应力随壁厚变化等因素。
{"title":"Experimental investigation of filament-wound composite tubes for mechanical characterization by internal pressure testing","authors":"T. Rasheed, S. Akbar, S. Mirza","doi":"10.1109/IBCAST.2013.6512125","DOIUrl":"https://doi.org/10.1109/IBCAST.2013.6512125","url":null,"abstract":"This paper presents method for the characterization of composite tubes produced by filament winding technique. The aim of this study is to investigate the mechanical properties by tensile test and under internal pressure loads. For this purpose specimens produced with different orientation having the same reinforcement with two different matrix systems. Data produced experimentally by measuring the mechanical properties like longitudinal tensile and hoop tensile properties, strain in hoop direction and maximum hoop stresses during the hydraulic testing. In order to investigate these parameters, internal pressure tests are done on the filament-wound composite tubes having internal diameter 64.5± 0.5 mm and length 320± 2.0 mm according to ASTM D 1599-99 standard. The tubes for the testing are manufactured by wet filament winding methods of [± 60°] E-glass/Epoxy of various wall thicknesses. Hydraulic tests revealed that the tubes with winding orientation [± 60°]2[±90°]2 exhibits better burst performance compared with others orientations. In addition, factors affecting the behavior of the tubes like buckling, stress variation through wall thickness are discussed.","PeriodicalId":276834,"journal":{"name":"Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)","volume":"40 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133694427","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 : 2013-05-02DOI: 10.1109/IBCAST.2013.6512163
S. Mushtaq, R. Basit
To model the Multiphase flow along with phase transition process is a challenging task. In the present paper, capability of Lattice Boltzmann method (LBM) to simulate flow through complex geometries and multiphase flow has been discussed. LBM is an innovative computational fluid dynamics (CFD) approach based on kinetic models. It describes the physical system as an artificial micro-world of the particles in which the particles simply propagate, collide and interact. To check the validity of LBM, simulations have been performed for two dimensional Poisuelle flow as a test problem and compared with analytical result. Then simulations results for various geometries resembling the porous media, introduced in the flow have also been presented. For the simulation of multiphase flow involving phase transition Shan and Chen model has been used. Periodic boundary conditions have been applied in all directions. Then gravity has been introduced as the driving force. Phase transition occur spontaneously whenever the interaction strength between the particles exceeds its threshold limit. Results have been verified by Laplace law. Finally, it has been concluded that LBM is a simulation method of choice for simulating flow through porous media and multiphase flow.
{"title":"Multiphase flow modeling using Lattice Boltzmann method","authors":"S. Mushtaq, R. Basit","doi":"10.1109/IBCAST.2013.6512163","DOIUrl":"https://doi.org/10.1109/IBCAST.2013.6512163","url":null,"abstract":"To model the Multiphase flow along with phase transition process is a challenging task. In the present paper, capability of Lattice Boltzmann method (LBM) to simulate flow through complex geometries and multiphase flow has been discussed. LBM is an innovative computational fluid dynamics (CFD) approach based on kinetic models. It describes the physical system as an artificial micro-world of the particles in which the particles simply propagate, collide and interact. To check the validity of LBM, simulations have been performed for two dimensional Poisuelle flow as a test problem and compared with analytical result. Then simulations results for various geometries resembling the porous media, introduced in the flow have also been presented. For the simulation of multiphase flow involving phase transition Shan and Chen model has been used. Periodic boundary conditions have been applied in all directions. Then gravity has been introduced as the driving force. Phase transition occur spontaneously whenever the interaction strength between the particles exceeds its threshold limit. Results have been verified by Laplace law. Finally, it has been concluded that LBM is a simulation method of choice for simulating flow through porous media and multiphase flow.","PeriodicalId":276834,"journal":{"name":"Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130982557","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 : 2013-05-02DOI: 10.1109/IBCAST.2013.6512160
M. Arshad, I. R. Chughtai, M. H. Inayat, A. Haq
Rectangular shaped sieve plate column was installed for study of transport parameters through high speed photography and image analysis. Two Immiscible liquids consisting of the dispersed phase (water) and continuous phase (kerosene oil) were introduced in countercurrent operation. Experiments were performed for dispersed and continuous phase superficial velocities 0.16-0.44 cm/sec and 0.37-0.47 cm/sec respectively, pulsation frequency 0.95 -1.72 rev/sec and pulsation amplitude 1cm. Upon increasing the superficial velocity of dispersed phase, its void fraction increases up to its asymptotic value and droplet velocity increase while the droplet size decreases. Upon increasing the pulsation frequency, its void fraction increases while the droplet size and droplet velocity decreases. A Computational Multi Fluid Dynamics simulation has been carried out in order to verify the experimental results using the FLUENT. The CMFD calculations for void fraction have been compared with the experimental results which have shown a maximum deviation of 2-3%.
{"title":"Experimental study and CMFD modeling of transport processes in flow of two Immiscible liquids","authors":"M. Arshad, I. R. Chughtai, M. H. Inayat, A. Haq","doi":"10.1109/IBCAST.2013.6512160","DOIUrl":"https://doi.org/10.1109/IBCAST.2013.6512160","url":null,"abstract":"Rectangular shaped sieve plate column was installed for study of transport parameters through high speed photography and image analysis. Two Immiscible liquids consisting of the dispersed phase (water) and continuous phase (kerosene oil) were introduced in countercurrent operation. Experiments were performed for dispersed and continuous phase superficial velocities 0.16-0.44 cm/sec and 0.37-0.47 cm/sec respectively, pulsation frequency 0.95 -1.72 rev/sec and pulsation amplitude 1cm. Upon increasing the superficial velocity of dispersed phase, its void fraction increases up to its asymptotic value and droplet velocity increase while the droplet size decreases. Upon increasing the pulsation frequency, its void fraction increases while the droplet size and droplet velocity decreases. A Computational Multi Fluid Dynamics simulation has been carried out in order to verify the experimental results using the FLUENT. The CMFD calculations for void fraction have been compared with the experimental results which have shown a maximum deviation of 2-3%.","PeriodicalId":276834,"journal":{"name":"Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)","volume":"115 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134430423","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 : 2013-05-02DOI: 10.1109/IBCAST.2013.6512184
I. Hussain, A. K. Rashid, H. Ullah
This paper presents a new hybrid type of phase shifter that employs basic Schiffman lines. Compared with conventional coupled line and Schiffman line phase shifters the new hybrid design shows advantage of optimally very small phase shift error of (±5°) over an entire band of 2.85-17.15 GHz (143% bandwidth). To validate the method, a 90° phase shifter is designed and simulated.
{"title":"Hybrid type of broad-band microwave phase shifter using schiffman lines","authors":"I. Hussain, A. K. Rashid, H. Ullah","doi":"10.1109/IBCAST.2013.6512184","DOIUrl":"https://doi.org/10.1109/IBCAST.2013.6512184","url":null,"abstract":"This paper presents a new hybrid type of phase shifter that employs basic Schiffman lines. Compared with conventional coupled line and Schiffman line phase shifters the new hybrid design shows advantage of optimally very small phase shift error of (±5°) over an entire band of 2.85-17.15 GHz (143% bandwidth). To validate the method, a 90° phase shifter is designed and simulated.","PeriodicalId":276834,"journal":{"name":"Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)","volume":"8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133038110","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 : 2013-05-02DOI: 10.1109/IBCAST.2013.6512158
M. Ozair, M. N. Qureshi
It has been broadly reported in the literature that the large segmented solid rocket motors (SRMs), such as Ariane 5 solid booster (P230) and Space Shuttle RSRM (Re-designed SRM), experience undesirable pressure oscillations that lead to thrust oscillations during combustion due to a complex coupling between the combustion and the internal aerodynamics of the combustion chamber. These fluctuations adversely affect the rocket motor performance, could damage the payload and eventually cause mission failure. To investigate these instabilities, experiments on full-size motors are very expensive, complicated and time consuming, and are therefore not really suited for research. In this paper, LP6 motor, the 1/15- scale axisymmetric model of the Ariane 5 booster, is used to study the pressure oscillations and the vortex-shedding induced pressure instabilities. Computational Fluid Dynamics (CFD) simulations were carried out on a quadrilateral mesh of the LP6 geometry at the time of 6.4 s after ignition when the pressure oscillations were found to be almost peaked. Pressure oscillation frequencies and amplitudes obtained from CFD simulations are found to be in good agreement with experimental results obtained at ONERA (French National Aerospace Research Centre). From CFD simulations, it was also found that the potential source of instabilities and pressure oscillations in LP6 motor having no inhibitor rings or restrictors is the surface vortex shedding mechanism which is a phenomenon that has also been observed in the experiments. On the basis of the present study and results, CFD simulations can also be carried out for different geometric configurations and flow conditions in other SRMs to investigate the instabilities and pressure oscillations occurring in their combustion chambers.
{"title":"Numerical simulation of pressure oscillations and instabilities in a solid propellant subscale motor","authors":"M. Ozair, M. N. Qureshi","doi":"10.1109/IBCAST.2013.6512158","DOIUrl":"https://doi.org/10.1109/IBCAST.2013.6512158","url":null,"abstract":"It has been broadly reported in the literature that the large segmented solid rocket motors (SRMs), such as Ariane 5 solid booster (P230) and Space Shuttle RSRM (Re-designed SRM), experience undesirable pressure oscillations that lead to thrust oscillations during combustion due to a complex coupling between the combustion and the internal aerodynamics of the combustion chamber. These fluctuations adversely affect the rocket motor performance, could damage the payload and eventually cause mission failure. To investigate these instabilities, experiments on full-size motors are very expensive, complicated and time consuming, and are therefore not really suited for research. In this paper, LP6 motor, the 1/15- scale axisymmetric model of the Ariane 5 booster, is used to study the pressure oscillations and the vortex-shedding induced pressure instabilities. Computational Fluid Dynamics (CFD) simulations were carried out on a quadrilateral mesh of the LP6 geometry at the time of 6.4 s after ignition when the pressure oscillations were found to be almost peaked. Pressure oscillation frequencies and amplitudes obtained from CFD simulations are found to be in good agreement with experimental results obtained at ONERA (French National Aerospace Research Centre). From CFD simulations, it was also found that the potential source of instabilities and pressure oscillations in LP6 motor having no inhibitor rings or restrictors is the surface vortex shedding mechanism which is a phenomenon that has also been observed in the experiments. On the basis of the present study and results, CFD simulations can also be carried out for different geometric configurations and flow conditions in other SRMs to investigate the instabilities and pressure oscillations occurring in their combustion chambers.","PeriodicalId":276834,"journal":{"name":"Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)","volume":"5 4","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132340240","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 : 2013-05-02DOI: 10.1109/IBCAST.2013.6512141
U. Javed, M. Riaz, T. A. Cheema, H. Zafar
Lung tumor detection using Contrast Enhanced (CE) Computed Tomography (CT) images plays a key role in computer aided diagnosis and medical practice. Detection of a lung tumor and accurate segmentation is a very challenging task. One major task is to perform classification between a normal (healthy) lung tissue and abnormal (tumor) tissue. However this distribution of data is nonlinear and training a classifier on this kind of data is a difficult process. Limitation of existing approaches is that they assign equal importance to each input feature; this weight assessment is not true for all problems. In this paper we propose a novel method for assigning optimal weights for the calculated features. This proposed technique is tested on CE CT Lung images. Simulation results and analysis showed that our proposed system has shown better classification accuracy than the conventional SVM.
{"title":"Detection of lung tumor in CE CT images by using weighted Support Vector Machines","authors":"U. Javed, M. Riaz, T. A. Cheema, H. Zafar","doi":"10.1109/IBCAST.2013.6512141","DOIUrl":"https://doi.org/10.1109/IBCAST.2013.6512141","url":null,"abstract":"Lung tumor detection using Contrast Enhanced (CE) Computed Tomography (CT) images plays a key role in computer aided diagnosis and medical practice. Detection of a lung tumor and accurate segmentation is a very challenging task. One major task is to perform classification between a normal (healthy) lung tissue and abnormal (tumor) tissue. However this distribution of data is nonlinear and training a classifier on this kind of data is a difficult process. Limitation of existing approaches is that they assign equal importance to each input feature; this weight assessment is not true for all problems. In this paper we propose a novel method for assigning optimal weights for the calculated features. This proposed technique is tested on CE CT Lung images. Simulation results and analysis showed that our proposed system has shown better classification accuracy than the conventional SVM.","PeriodicalId":276834,"journal":{"name":"Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)","volume":"11 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123855252","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 : 2013-05-02DOI: 10.1109/IBCAST.2013.6512130
M. Asad, S. Iqbal, A. I. Bhatti
In this work a new reaching law (RL) is proposed that uses inverse hyperbolic function (IHF) instead of the Signum function for switching. The characteristic of this reaching law is that its switching gain is variable, during the reaching phase, which is governed by the parameters of IHF. Its gain decreases with the convergence of system states towards the sliding surface. The variable gain results in: (a) the considerable reduction of the phenomenon of chattering at the control inputs and (b) the decrease of the reaching phase of the sliding mode control (SMC).
{"title":"MIMO sliding mode controller design using inverse hyperbolic function","authors":"M. Asad, S. Iqbal, A. I. Bhatti","doi":"10.1109/IBCAST.2013.6512130","DOIUrl":"https://doi.org/10.1109/IBCAST.2013.6512130","url":null,"abstract":"In this work a new reaching law (RL) is proposed that uses inverse hyperbolic function (IHF) instead of the Signum function for switching. The characteristic of this reaching law is that its switching gain is variable, during the reaching phase, which is governed by the parameters of IHF. Its gain decreases with the convergence of system states towards the sliding surface. The variable gain results in: (a) the considerable reduction of the phenomenon of chattering at the control inputs and (b) the decrease of the reaching phase of the sliding mode control (SMC).","PeriodicalId":276834,"journal":{"name":"Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)","volume":"48 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121323435","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 : 2013-05-02DOI: 10.1109/IBCAST.2013.6512182
H. Nawaz, M. Rizwan
The paper presents an InAlAs/InGaAs Hetero-junction Bi-polar transistor structure. The structure formation and performance analysis has been carried out using SILVACO software. Parametric analysis is carried out and results are presented in correspondence with the theory. Doping profile of proposed HBT is optimized to achieve appropriate current gain and maintain possibly low resistance in the base region to avoid recombination. Emitter area of 5×5 μm2 is used to achieve low off set voltage and high gain of 62dB while low doping enabled the device to operate effectively at high frequencies that is up-till 80GHz. Energy band diagram and effects of different layers are discussed showing efficient workability of the proposed structure.
{"title":"Design and analysis of two-dimensional InAlAs/InGaAs Single Hetero-junction Bipolar Transistor","authors":"H. Nawaz, M. Rizwan","doi":"10.1109/IBCAST.2013.6512182","DOIUrl":"https://doi.org/10.1109/IBCAST.2013.6512182","url":null,"abstract":"The paper presents an InAlAs/InGaAs Hetero-junction Bi-polar transistor structure. The structure formation and performance analysis has been carried out using SILVACO software. Parametric analysis is carried out and results are presented in correspondence with the theory. Doping profile of proposed HBT is optimized to achieve appropriate current gain and maintain possibly low resistance in the base region to avoid recombination. Emitter area of 5×5 μm2 is used to achieve low off set voltage and high gain of 62dB while low doping enabled the device to operate effectively at high frequencies that is up-till 80GHz. Energy band diagram and effects of different layers are discussed showing efficient workability of the proposed structure.","PeriodicalId":276834,"journal":{"name":"Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)","volume":"68 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116344523","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 : 2013-05-02DOI: 10.1109/IBCAST.2013.6512192
N. Ahsan, Z. Haider, S. Sultan
This paper presents a new scheme for the range estimation of an unknown radar emitter. With the proposed algorithm, range of unknown radar emitter can be determined by amplitude comparison of closely spaced time samples. A mathematical model of this ranging method is discussed in detail and supported by computer simulations. For various scenarios, the standard deviation in range estimate has been estimated. For normal incidence, the simulation results indicate that standard deviation in range estimate is only 76m for a 20Km range considering 10dB SNR and observer position error of ±1m. The comparison of proposed method with traditional triangulation method has also been presented. The comparison indicates that for a single platform configuration, the proposed scheme provides more accurate range estimation in a short span of time. Therefore, making it a suitable choice for applications where fast update is required.
{"title":"Ranging using amplitude comparison of closely spaced time samples","authors":"N. Ahsan, Z. Haider, S. Sultan","doi":"10.1109/IBCAST.2013.6512192","DOIUrl":"https://doi.org/10.1109/IBCAST.2013.6512192","url":null,"abstract":"This paper presents a new scheme for the range estimation of an unknown radar emitter. With the proposed algorithm, range of unknown radar emitter can be determined by amplitude comparison of closely spaced time samples. A mathematical model of this ranging method is discussed in detail and supported by computer simulations. For various scenarios, the standard deviation in range estimate has been estimated. For normal incidence, the simulation results indicate that standard deviation in range estimate is only 76m for a 20Km range considering 10dB SNR and observer position error of ±1m. The comparison of proposed method with traditional triangulation method has also been presented. The comparison indicates that for a single platform configuration, the proposed scheme provides more accurate range estimation in a short span of time. Therefore, making it a suitable choice for applications where fast update is required.","PeriodicalId":276834,"journal":{"name":"Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)","volume":"299 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115613464","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 : 2013-05-02DOI: 10.1109/IBCAST.2013.6512175
U. Hamid, H. Shahzad, M. Irfan
This paper presents Fast Fourier Transform (FFT) benchmark results to measure and compare the performance of various DSP and Intel processors for underwater signal processing applications. This paper aims to show performance enhancement in Intel processors as compared to DSP processors by using parallel programming for implementing signal processing functions in real time. This paper provides results that show a significant decrease in FFT execution time on an Intel based Multicore processor using parallel programming. Therefore comparative analysis among different processor architectures presented in this paper will help the system designers in selecting an optimal processor for underwater signal processing applications.
{"title":"Comparative analysis of DSP and intel processors by implementing FFTs using parallel programming for underwater signal processing applications","authors":"U. Hamid, H. Shahzad, M. Irfan","doi":"10.1109/IBCAST.2013.6512175","DOIUrl":"https://doi.org/10.1109/IBCAST.2013.6512175","url":null,"abstract":"This paper presents Fast Fourier Transform (FFT) benchmark results to measure and compare the performance of various DSP and Intel processors for underwater signal processing applications. This paper aims to show performance enhancement in Intel processors as compared to DSP processors by using parallel programming for implementing signal processing functions in real time. This paper provides results that show a significant decrease in FFT execution time on an Intel based Multicore processor using parallel programming. Therefore comparative analysis among different processor architectures presented in this paper will help the system designers in selecting an optimal processor for underwater signal processing applications.","PeriodicalId":276834,"journal":{"name":"Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)","volume":"34 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126162233","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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