Search Results for "propeller design"
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Showing 4 open source projects for "propeller design"
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Propeller
Develop more, Code less. Propeller is a front-end responsive framework
Propeller is a front-end responsive framework based on Google’s Material Design Standards & Bootstrap. Library with 25 Responsive UI Components. Ready to use template which speeds up the Development process. Detailed User Manual which provides step by step usage for every Propeller component. The downloaded folder will have following directories and files, with a logical grouping of common assets including both compiled and minified versions. Just copy the compiled CSS and JS files and the font... -
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DACPEI
Conceptual design of Light Fixed Wing Aircraft
DACPEI is a WYSIWUG Software for Conceptual design of Light Fixed Wing aircraft. It is specifically designed to be intuitive and easy to use by engineering students (not necessary aerospace/aeronautics). DACPEI is divided in 9 modules, for analyzing mission profile, Aircraft performance, propulsion and layout design, as well as sketch component for developing aircraft drawings. DACPEI enable users to export their design to the FlightGear flight simulator software, enabling the designer... -
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freeship-plus-in-lazarus
design and calculations of hydrodynamics of vessels
... for the full parametric analysis of resistance and power prediction for a ship and other calculations of hydrodynamics of vessels and underwater vehicles. FREE!ship Plus allows the designer to simulate and analyze condition of balance of a complex completely hull - rudders - keels - engine - propellers in different regimes and of service conditions of a ship. The analyzable system includes a hull, appendages, a propeller and the engine (i.e. resistance, power, a thrust and a torque), and also var -
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Single Rotor Vertical Take-off and Landing system is selected due to complexity and enthralling factor. Aim of the project is to design an Unmanned Aerial Vehicle which can take off and land vertically with using single propeller in order to provide thrust. Challenge involved in the system is single rotating propeller which is main contributing element to provide lift is making the whole system unstable due to torque of power system. In case of conventional helicopter tail rotor is provided...
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