Abstract

 Technology has the enemy of nature in one way .But sometimes technologies do come out as an exception to the above rule. Technological advancements have improvised them over time. A Load Carry Aerial vehicle (LCAV) helps overcome the labor problems. This project is based on Load Carry aerial vehicle which used to carry the various types of load (light load, heavy load and water bottle). The LCAV hover using Coanda effect principle. The LCAV works using Coanda effect principle with multi rotor and also its works on vertical takeoff and landing technique. Vertical Takeoff and Landing (VTOL) flight has been one of the main interests of both the civilian and military aviation communities throughout the history of flight. Today, several aircraft capable of achieving V/STOL flight exist. But it is entirely different from VTOL aircraft or helicopter or multi copters (tri copter, quarter copter or hexa copter). In LCAV there is no big rotor like on a helicopter and the flight is very stable and safe for the surrounding. In this project we shall carryout the designing of LCAV using CATIA. Then flow characteristic can be take using Computational fluid dynamics software ANSYS.

Authors and Affiliations