ºÝºÝߣshows by User: pawanrm1 / http://www.slideshare.net/images/logo.gif ºÝºÝߣshows by User: pawanrm1 / Tue, 12 May 2015 11:32:14 GMT ºÝºÝߣShare feed for ºÝºÝߣshows by User: pawanrm1 Conceptual Design of Blended Wing Body Cargo Aircraft /slideshow/conceptual-design-of-blended-wing-body-cargo-aircraft/48043323 bwbdesign02-150512113214-lva1-app6891
A Blended Wing Body (BWB) aircraft is a configuration where the wing and fuselage are integrated which essentially results in a large flying wing. BWB aircraft were previously called ‘tailless airplanes’ and ‘Flying-Wing aircraft’. The BWB configuration has shown promise in terms of aerodynamic efficiency, in particular for very large transport aircraft, because the configuration has a single lifting surface that means an aerodynamically clean configuration.]]>

A Blended Wing Body (BWB) aircraft is a configuration where the wing and fuselage are integrated which essentially results in a large flying wing. BWB aircraft were previously called ‘tailless airplanes’ and ‘Flying-Wing aircraft’. The BWB configuration has shown promise in terms of aerodynamic efficiency, in particular for very large transport aircraft, because the configuration has a single lifting surface that means an aerodynamically clean configuration.]]>
Tue, 12 May 2015 11:32:14 GMT /slideshow/conceptual-design-of-blended-wing-body-cargo-aircraft/48043323 pawanrm1@slideshare.net(pawanrm1) Conceptual Design of Blended Wing Body Cargo Aircraft pawanrm1 A Blended Wing Body (BWB) aircraft is a configuration where the wing and fuselage are integrated which essentially results in a large flying wing. BWB aircraft were previously called ‘tailless airplanes’ and ‘Flying-Wing aircraft’. The BWB configuration has shown promise in terms of aerodynamic efficiency, in particular for very large transport aircraft, because the configuration has a single lifting surface that means an aerodynamically clean configuration. <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/bwbdesign02-150512113214-lva1-app6891-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br> A Blended Wing Body (BWB) aircraft is a configuration where the wing and fuselage are integrated which essentially results in a large flying wing. BWB aircraft were previously called ‘tailless airplanes’ and ‘Flying-Wing aircraft’. The BWB configuration has shown promise in terms of aerodynamic efficiency, in particular for very large transport aircraft, because the configuration has a single lifting surface that means an aerodynamically clean configuration.
Conceptual Design of Blended Wing Body Cargo Aircraft from TechWorksLab Private Limited
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DESIGN OPTIMIZATION OF WIND TURBINE BLADE /slideshow/wind-turbine-design/47957907 windturbinedesign-150510064608-lva1-app6891
The objective of this project is to design a wind turbine that is optimized for the constraints that come with residential use. The main tasks of this project are: > To study the design process and methodology of wind turbine > Derive the Blade Element Momentum (BEM) theory then use it to conduct a parametric study that will determine if the optimized values of blade pitch and chord length create the most efficient blade geometry > Analyse different air-foils to determine which one creates the most efficient wind turbine blade.]]>

The objective of this project is to design a wind turbine that is optimized for the constraints that come with residential use. The main tasks of this project are: > To study the design process and methodology of wind turbine > Derive the Blade Element Momentum (BEM) theory then use it to conduct a parametric study that will determine if the optimized values of blade pitch and chord length create the most efficient blade geometry > Analyse different air-foils to determine which one creates the most efficient wind turbine blade.]]>
Sun, 10 May 2015 06:46:08 GMT /slideshow/wind-turbine-design/47957907 pawanrm1@slideshare.net(pawanrm1) DESIGN OPTIMIZATION OF WIND TURBINE BLADE pawanrm1 The objective of this project is to design a wind turbine that is optimized for the constraints that come with residential use. The main tasks of this project are: > To study the design process and methodology of wind turbine > Derive the Blade Element Momentum (BEM) theory then use it to conduct a parametric study that will determine if the optimized values of blade pitch and chord length create the most efficient blade geometry > Analyse different air-foils to determine which one creates the most efficient wind turbine blade. <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/windturbinedesign-150510064608-lva1-app6891-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br> The objective of this project is to design a wind turbine that is optimized for the constraints that come with residential use. The main tasks of this project are: &gt; To study the design process and methodology of wind turbine &gt; Derive the Blade Element Momentum (BEM) theory then use it to conduct a parametric study that will determine if the optimized values of blade pitch and chord length create the most efficient blade geometry &gt; Analyse different air-foils to determine which one creates the most efficient wind turbine blade.
DESIGN OPTIMIZATION OF WIND TURBINE BLADE from TechWorksLab Private Limited
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HELIOCENTRIC and GEOCENTRIC Systems /slideshow/heliocentric-and-geocentric-systems/47087518 heliocentricvsgeocentric-150416150931-conversion-gate02
Heliocentric Systems, Geocentric Systems, # Frame of reference]]>

Heliocentric Systems, Geocentric Systems, # Frame of reference]]>
Thu, 16 Apr 2015 15:09:31 GMT /slideshow/heliocentric-and-geocentric-systems/47087518 pawanrm1@slideshare.net(pawanrm1) HELIOCENTRIC and GEOCENTRIC Systems pawanrm1 Heliocentric Systems, Geocentric Systems, # Frame of reference <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/heliocentricvsgeocentric-150416150931-conversion-gate02-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br> Heliocentric Systems, Geocentric Systems, # Frame of reference
HELIOCENTRIC and GEOCENTRIC Systems from TechWorksLab Private Limited
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CRYOGENIC ROCKET ENGINE /slideshow/cryogenic-rocket-engine-45694341/45694341 cre009-150311034004-conversion-gate01
Cryogenics is the study of the operations at very low temperature (below −150 °C, −238 °F or 123 K) and the behaviour of materials at these temperatures.]]>

Cryogenics is the study of the operations at very low temperature (below −150 °C, −238 °F or 123 K) and the behaviour of materials at these temperatures.]]>
Wed, 11 Mar 2015 03:40:04 GMT /slideshow/cryogenic-rocket-engine-45694341/45694341 pawanrm1@slideshare.net(pawanrm1) CRYOGENIC ROCKET ENGINE pawanrm1 Cryogenics is the study of the operations at very low temperature (below −150 °C, −238 °F or 123 K) and the behaviour of materials at these temperatures. <img style="border:1px solid #C3E6D8;float:right;" alt="" src="https://cdn.slidesharecdn.com/ss_thumbnails/cre009-150311034004-conversion-gate01-thumbnail.jpg?width=120&amp;height=120&amp;fit=bounds" /><br> Cryogenics is the study of the operations at very low temperature (below −150 °C, −238 °F or 123 K) and the behaviour of materials at these temperatures.
CRYOGENIC ROCKET ENGINE from TechWorksLab Private Limited
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https://cdn.slidesharecdn.com/profile-photo-pawanrm1-48x48.jpg?cb=1741070652 pawan.xyz https://cdn.slidesharecdn.com/ss_thumbnails/bwbdesign02-150512113214-lva1-app6891-thumbnail.jpg?width=320&height=320&fit=bounds slideshow/conceptual-design-of-blended-wing-body-cargo-aircraft/48043323 Conceptual Design of B... https://cdn.slidesharecdn.com/ss_thumbnails/windturbinedesign-150510064608-lva1-app6891-thumbnail.jpg?width=320&height=320&fit=bounds slideshow/wind-turbine-design/47957907 DESIGN OPTIMIZATION OF... https://cdn.slidesharecdn.com/ss_thumbnails/heliocentricvsgeocentric-150416150931-conversion-gate02-thumbnail.jpg?width=320&height=320&fit=bounds slideshow/heliocentric-and-geocentric-systems/47087518 HELIOCENTRIC and GEOCE...