Showing 4 open source projects for "propeller design"

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  • 1
    Propeller

    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.
    Downloads: 0 This Week
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  • 2
    DACPEI

    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 to...
    Downloads: 0 This Week
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  • 3

    freeship-plus-in-lazarus

    design and calculations of hydrodynamics of vessels

    THE PROJECT IS MOVED TO GitHub https://github.com/markmal/freeship-plus-in-lazarus FREE!ship Plus in Lazarus is further development of the FREE!ship Plus (by http://www.hydronship.net) Windows program with free source code FREE!ship v3.x under license GNU GPL. This FREE!ship Plus application is migrated into free open source Lazarus / Free Pascal environment to promote further development in various platforms and for various platforms (OS and architectures). FREE!ship Plus is designed...
    Downloads: 0 This Week
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  • 4
    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 to balance the torque provided by main rotor power system again multi rotors have even number ofrotating propellers which rotates in such fashion cancels the net moment about body. ...
    Downloads: 0 This Week
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