Design And Analysis Of UAV Wing Landing Gear Interface
| dc.contributor.author | Prasanna Venkatesan, S | |
| dc.contributor.author | Rajesh, T | |
| dc.contributor.author | Abhishek, Reddy | |
| dc.date.accessioned | 2015-12-28T14:19:34Z | |
| dc.date.available | 2015-12-28T14:19:34Z | |
| dc.date.issued | 2015-12-28T14:19:34Z | |
| dc.description.abstract | Unmanned Ariel Vehicle (UAV) is becoming an essential part of airpower as well as air surveillance of every nation. Previously they were mainly used for air surveillance in high security regions as well as in disaster struck region. Recently they are being deployed for traffic surveillance and monitoring and even used for combat purposes in hostile regions. This helps in reducing loss of lives and cost during mishaps. They are also used as flying targets for testing Surface to Air Missiles (SAMs). The UAVs are piloted remotely through ground stations or through other in flight controls. Some UAVs are developed to be selfguided. The project deals with design and analysis of wing-engine frame-landing gear interface for UAV. The landing gear interface is used for joining the engine frame with landing gear to the center section of the wings through metallic ribs. The project deals with designing the mounting interfaces and solid mapping the interfaces (3D mesh) and detailed local static analysis of the interface for design load. | en_US |
| dc.identifier.uri | http://hdl.handle.net/123456789/5531 | |
| dc.language.iso | en | en_US |
| dc.subject | Design And Analysis Of UAV Wing Landing Gear Interface | en_US |
| dc.subject | Prasanna Venkatesan S | en_US |
| dc.subject | Rajesh T | en_US |
| dc.subject | Abhishek Reddy | en_US |
| dc.title | Design And Analysis Of UAV Wing Landing Gear Interface | en_US |
| dc.type | Thesis | en_US |