際際滷shows by User: shameem.mist / http://www.slideshare.net/images/logo.gif 際際滷shows by User: shameem.mist / Fri, 09 Sep 2011 12:08:24 GMT 際際滷Share feed for 際際滷shows by User: shameem.mist Fluid motion in the posterior chamber of the eye /slideshow/fluid-motion-in-the-posterior-chamber-of-the-eye/9195325 fluidmotionintheposteriorchamberoftheeye-110909120827-phpapp01
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]]> Fri, 09 Sep 2011 12:08:24 GMT /slideshow/fluid-motion-in-the-posterior-chamber-of-the-eye/9195325 shameem.mist@slideshare.net(shameem.mist) Fluid motion in the posterior chamber of the eye shameem.mist <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/fluidmotionintheposteriorchamberoftheeye-110909120827-phpapp01-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br>
Fluid motion in the posterior chamber of the eye from Dr. Bhuiyan S. M. Ebna Hai
]]> 3268 6 https://cdn.slidesharecdn.com/ss_thumbnails/fluidmotionintheposteriorchamberoftheeye-110909120827-phpapp01-thumbnail.jpg?width=120&height=120&fit=bounds document White http://activitystrea.ms/schema/1.0/post http://activitystrea.ms/schema/1.0/posted 0 A simple model of the liver microcirculation /slideshow/a-simple-model-of-the-liver-microcirculation/9195300 asimplemodelofthelivermicrocirculation-110909120620-phpapp01
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]]> Fri, 09 Sep 2011 12:06:19 GMT /slideshow/a-simple-model-of-the-liver-microcirculation/9195300 shameem.mist@slideshare.net(shameem.mist) A simple model of the liver microcirculation shameem.mist <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/asimplemodelofthelivermicrocirculation-110909120620-phpapp01-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br>
A simple model of the liver microcirculation from Dr. Bhuiyan S. M. Ebna Hai
]]> 2473 8 https://cdn.slidesharecdn.com/ss_thumbnails/asimplemodelofthelivermicrocirculation-110909120620-phpapp01-thumbnail.jpg?width=120&height=120&fit=bounds document White http://activitystrea.ms/schema/1.0/post http://activitystrea.ms/schema/1.0/posted 0 Study of wind effect on building with hexagonal cross section /slideshow/study-of-wind-effect-on-building-with-hexagonal-cross-section/9195274 studyofwindeffectonbuildingwithhexagonalcross-section-110909120347-phpapp01
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]]> Fri, 09 Sep 2011 12:03:44 GMT /slideshow/study-of-wind-effect-on-building-with-hexagonal-cross-section/9195274 shameem.mist@slideshare.net(shameem.mist) Study of wind effect on building with hexagonal cross section shameem.mist <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/studyofwindeffectonbuildingwithhexagonalcross-section-110909120347-phpapp01-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br>
Study of wind effect on building with hexagonal cross section from Dr. Bhuiyan S. M. Ebna Hai
]]> 3476 4 https://cdn.slidesharecdn.com/ss_thumbnails/studyofwindeffectonbuildingwithhexagonalcross-section-110909120347-phpapp01-thumbnail.jpg?width=120&height=120&fit=bounds document White http://activitystrea.ms/schema/1.0/post http://activitystrea.ms/schema/1.0/posted 0 Dynamic behavior of catalytic converters /slideshow/dynamic-behavior-of-catalytic-converters/9195252 dynamicbehaviorofcatalyticconverters-110909120128-phpapp01
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]]> Fri, 09 Sep 2011 12:01:25 GMT /slideshow/dynamic-behavior-of-catalytic-converters/9195252 shameem.mist@slideshare.net(shameem.mist) Dynamic behavior of catalytic converters shameem.mist <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/dynamicbehaviorofcatalyticconverters-110909120128-phpapp01-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br>
Dynamic behavior of catalytic converters from Dr. Bhuiyan S. M. Ebna Hai
]]> 4609 8 https://cdn.slidesharecdn.com/ss_thumbnails/dynamicbehaviorofcatalyticconverters-110909120128-phpapp01-thumbnail.jpg?width=120&height=120&fit=bounds document White http://activitystrea.ms/schema/1.0/post http://activitystrea.ms/schema/1.0/posted 0 Engineering Drawing /slideshow/engineering-drawing/1094885 engineeringdrawingi-090303074237-phpapp01
Download link: https://www.researchgate.net/publication/318852873_Engineering_Drawing_-_I DOI: 10.13140/RG.2.2.22512.56328 An engineering drawing is a type of technical drawing, used to fully and clearly define requirements for engineered items, and is usually created in accordance with standardized conventions for layout, nomenclature, interpretation, appearance size, etc. Its purpose is to accurately and unambiguously capture all the geometric features of a product or a component. The end goal of an engineering drawing is to convey all the required information that will allow a manufacturer to produce that component.]]>
Download link: https://www.researchgate.net/publication/318852873_Engineering_Drawing_-_I DOI: 10.13140/RG.2.2.22512.56328 An engineering drawing is a type of technical drawing, used to fully and clearly define requirements for engineered items, and is usually created in accordance with standardized conventions for layout, nomenclature, interpretation, appearance size, etc. Its purpose is to accurately and unambiguously capture all the geometric features of a product or a component. The end goal of an engineering drawing is to convey all the required information that will allow a manufacturer to produce that component.]]> Tue, 03 Mar 2009 07:42:20 GMT /slideshow/engineering-drawing/1094885 shameem.mist@slideshare.net(shameem.mist) Engineering Drawing shameem.mist Download link: https://www.researchgate.net/publication/318852873_Engineering_Drawing_-_I DOI: 10.13140/RG.2.2.22512.56328 An engineering drawing is a type of technical drawing, used to fully and clearly define requirements for engineered items, and is usually created in accordance with standardized conventions for layout, nomenclature, interpretation, appearance size, etc. Its purpose is to accurately and unambiguously capture all the geometric features of a product or a component. The end goal of an engineering drawing is to convey all the required information that will allow a manufacturer to produce that component. <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/engineeringdrawingi-090303074237-phpapp01-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br> Download link: https://www.researchgate.net/publication/318852873_Engineering_Drawing_-_I DOI: 10.13140/RG.2.2.22512.56328 An engineering drawing is a type of technical drawing, used to fully and clearly define requirements for engineered items, and is usually created in accordance with standardized conventions for layout, nomenclature, interpretation, appearance size, etc. Its purpose is to accurately and unambiguously capture all the geometric features of a product or a component. The end goal of an engineering drawing is to convey all the required information that will allow a manufacturer to produce that component.
Engineering Drawing from Dr. Bhuiyan S. M. Ebna Hai
]]> 441973 219 https://cdn.slidesharecdn.com/ss_thumbnails/engineeringdrawingi-090303074237-phpapp01-thumbnail.jpg?width=120&height=120&fit=bounds presentation White http://activitystrea.ms/schema/1.0/post http://activitystrea.ms/schema/1.0/posted 0 Design Analysis Of Uav (Unmanned Air Vehicle) Using NACA 0012 Aerofoil Profile /slideshow/design-analysis-of-uav-unmanned-air-vehicle-using-naca-0012-aerofoil-profile/998520 design-analysis-of-uav-unmanned-air-vehicle-using-naca-0012-aerofoil-profile-1233944033882290-2
This research work is concerned with the application of conceptual design of Unmanned Air Vehicle (UAV). UAV is used for surveillance and reconnaissance to serve for the defense as well as national security and intelligence purpose. Here NACA 0012 aerofoil profile is used to design UAV by using CFD (Computational Fluid Dynamics) software. The aim of this research is to investigate the flow patterns and determine the aerodynamic characteristics of NACA 0012 profile by varying the angle of attack and Reynolds Number numerically. The research is carried out with symmetric aerofoil with the chord length of 0.1m. The research work explained different aerodynamic characteristics like lift force and drag force, lift and drag coefficient, pressure distribution over aerofoil etc.]]>
This research work is concerned with the application of conceptual design of Unmanned Air Vehicle (UAV). UAV is used for surveillance and reconnaissance to serve for the defense as well as national security and intelligence purpose. Here NACA 0012 aerofoil profile is used to design UAV by using CFD (Computational Fluid Dynamics) software. The aim of this research is to investigate the flow patterns and determine the aerodynamic characteristics of NACA 0012 profile by varying the angle of attack and Reynolds Number numerically. The research is carried out with symmetric aerofoil with the chord length of 0.1m. The research work explained different aerodynamic characteristics like lift force and drag force, lift and drag coefficient, pressure distribution over aerofoil etc.]]> Fri, 06 Feb 2009 12:19:01 GMT /slideshow/design-analysis-of-uav-unmanned-air-vehicle-using-naca-0012-aerofoil-profile/998520 shameem.mist@slideshare.net(shameem.mist) Design Analysis Of Uav (Unmanned Air Vehicle) Using NACA 0012 Aerofoil Profile shameem.mist This research work is concerned with the application of conceptual design of Unmanned Air Vehicle (UAV). UAV is used for surveillance and reconnaissance to serve for the defense as well as national security and intelligence purpose. Here NACA 0012 aerofoil profile is used to design UAV by using CFD (Computational Fluid Dynamics) software. The aim of this research is to investigate the flow patterns and determine the aerodynamic characteristics of NACA 0012 profile by varying the angle of attack and Reynolds Number numerically. The research is carried out with symmetric aerofoil with the chord length of 0.1m. The research work explained different aerodynamic characteristics like lift force and drag force, lift and drag coefficient, pressure distribution over aerofoil etc. <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/design-analysis-of-uav-unmanned-air-vehicle-using-naca-0012-aerofoil-profile-1233944033882290-2-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br> This research work is concerned with the application of conceptual design of Unmanned Air Vehicle (UAV). UAV is used for surveillance and reconnaissance to serve for the defense as well as national security and intelligence purpose. Here NACA 0012 aerofoil profile is used to design UAV by using CFD (Computational Fluid Dynamics) software. The aim of this research is to investigate the flow patterns and determine the aerodynamic characteristics of NACA 0012 profile by varying the angle of attack and Reynolds Number numerically. The research is carried out with symmetric aerofoil with the chord length of 0.1m. The research work explained different aerodynamic characteristics like lift force and drag force, lift and drag coefficient, pressure distribution over aerofoil etc.
Design Analysis Of Uav (Unmanned Air Vehicle) Using NACA 0012 Aerofoil Profile from Dr. Bhuiyan S. M. Ebna Hai
]]> 5612 4 https://cdn.slidesharecdn.com/ss_thumbnails/design-analysis-of-uav-unmanned-air-vehicle-using-naca-0012-aerofoil-profile-1233944033882290-2-thumbnail.jpg?width=120&height=120&fit=bounds document White http://activitystrea.ms/schema/1.0/post http://activitystrea.ms/schema/1.0/posted 0 Study of Aerodynamics of a Cricket Ball /slideshow/study-of-aerodynamics-of-a-cricket-ball/998421 study-of-aerodynamics-of-a-cricket-ball-1233941996979957-2
This research is concerned with the nature and aerodynamic behavior on cricket balls in flight. It is written to determine the aerodynamic characteristics of a cricket ball with a mass of 156 gm and approximate diameter of 70 mm, where a sample cricket ball was fixed with a shaft in a wind tunnel. The aerodynamic characteristics have been analyzed by varying the rotational rpm of the cricket ball, where the axis of rotation for seam and shaft is same and the pressure difference between the upper and the lower surface of the cricket ball determine by the help of static manometer. Some experimental works have also been carried out and compared with those of the results obtained numerically. The upward pressure, which creates lift, has increased almost linearly with the increase of ball position angle to approximately 15o to 30o and it also decrease with increase of ball rotational speed. Finally some conclusions have been drawn on the basis of the experimental result.]]>
This research is concerned with the nature and aerodynamic behavior on cricket balls in flight. It is written to determine the aerodynamic characteristics of a cricket ball with a mass of 156 gm and approximate diameter of 70 mm, where a sample cricket ball was fixed with a shaft in a wind tunnel. The aerodynamic characteristics have been analyzed by varying the rotational rpm of the cricket ball, where the axis of rotation for seam and shaft is same and the pressure difference between the upper and the lower surface of the cricket ball determine by the help of static manometer. Some experimental works have also been carried out and compared with those of the results obtained numerically. The upward pressure, which creates lift, has increased almost linearly with the increase of ball position angle to approximately 15o to 30o and it also decrease with increase of ball rotational speed. Finally some conclusions have been drawn on the basis of the experimental result.]]> Fri, 06 Feb 2009 11:56:48 GMT /slideshow/study-of-aerodynamics-of-a-cricket-ball/998421 shameem.mist@slideshare.net(shameem.mist) Study of Aerodynamics of a Cricket Ball shameem.mist This research is concerned with the nature and aerodynamic behavior on cricket balls in flight. It is written to determine the aerodynamic characteristics of a cricket ball with a mass of 156 gm and approximate diameter of 70 mm, where a sample cricket ball was fixed with a shaft in a wind tunnel. The aerodynamic characteristics have been analyzed by varying the rotational rpm of the cricket ball, where the axis of rotation for seam and shaft is same and the pressure difference between the upper and the lower surface of the cricket ball determine by the help of static manometer. Some experimental works have also been carried out and compared with those of the results obtained numerically. The upward pressure, which creates lift, has increased almost linearly with the increase of ball position angle to approximately 15o to 30o and it also decrease with increase of ball rotational speed. Finally some conclusions have been drawn on the basis of the experimental result. <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/study-of-aerodynamics-of-a-cricket-ball-1233941996979957-2-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br> This research is concerned with the nature and aerodynamic behavior on cricket balls in flight. It is written to determine the aerodynamic characteristics of a cricket ball with a mass of 156 gm and approximate diameter of 70 mm, where a sample cricket ball was fixed with a shaft in a wind tunnel. The aerodynamic characteristics have been analyzed by varying the rotational rpm of the cricket ball, where the axis of rotation for seam and shaft is same and the pressure difference between the upper and the lower surface of the cricket ball determine by the help of static manometer. Some experimental works have also been carried out and compared with those of the results obtained numerically. The upward pressure, which creates lift, has increased almost linearly with the increase of ball position angle to approximately 15o to 30o and it also decrease with increase of ball rotational speed. Finally some conclusions have been drawn on the basis of the experimental result.
Study of Aerodynamics of a Cricket Ball from Dr. Bhuiyan S. M. Ebna Hai
]]> 3069 7 https://cdn.slidesharecdn.com/ss_thumbnails/study-of-aerodynamics-of-a-cricket-ball-1233941996979957-2-thumbnail.jpg?width=120&height=120&fit=bounds document White http://activitystrea.ms/schema/1.0/post http://activitystrea.ms/schema/1.0/posted 0 https://cdn.slidesharecdn.com/profile-photo-shameem.mist-48x48.jpg?cb=1541520690 Bhuiyan Shameem Mahmood Ebna Hai was born in Dhaka, Bangladesh, in 1985. He has received B.Sc. degree in Mechanical Engineering from the Military Institute of Science and Technology under University of Dhaka, Bangladesh, in 2008, and achieved Erasmus Mundus M.Sc. degree in Mathematical Modelling in Engineering as well as M.Sc. in Industrial Mathematics from the University of Hamburg, Germany in 2012. He joined Helmut Schmidt University (University of the Federal Armed Forces Hamburg) as a Research Assistant at the Department of Mechanical Engineering in January 2013. His research interests include Numerical Simulation Techniques, Fluid Dynamics and Structural health monitoring (SHM) system. community.asme.org/members/ebnahai/default.aspx https://cdn.slidesharecdn.com/ss_thumbnails/fluidmotionintheposteriorchamberoftheeye-110909120827-phpapp01-thumbnail.jpg?width=320&height=320&fit=bounds slideshow/fluid-motion-in-the-posterior-chamber-of-the-eye/9195325 Fluid motion in the po... https://cdn.slidesharecdn.com/ss_thumbnails/asimplemodelofthelivermicrocirculation-110909120620-phpapp01-thumbnail.jpg?width=320&height=320&fit=bounds slideshow/a-simple-model-of-the-liver-microcirculation/9195300 A simple model of the ... https://cdn.slidesharecdn.com/ss_thumbnails/studyofwindeffectonbuildingwithhexagonalcross-section-110909120347-phpapp01-thumbnail.jpg?width=320&height=320&fit=bounds slideshow/study-of-wind-effect-on-building-with-hexagonal-cross-section/9195274 Study of wind effect o...