WING ANALYSIS OF A FLAPPING WING UNMANNED AERIAL VEHICLE USING CFD
| Author(s) | : | Purvi M. Joshi |
| Institution | : | ,Department of Mechanical engineering, Atmiya Institute of Technology &Science,Rajkot |
| Published In | : | Vol. 2, Issue 5 — May 2015 |
| Page No. | : | 216-221 |
| Domain | : | Engineering |
| Type | : | Research Paper |
| ISSN (Online) | : | 2348-4470 |
| ISSN (Print) | : | 2348-6406 |
:Traditional micro air vehicles (MAVs) are miniature version of full scale air craft from which their designprinciples closely follow. Non-traditional (UAVs) resemble to the design of birds or insects. A flapping wing modelhaving interaction of aerodynamics and inertial loading which can cause deformation of the wings is designed. Thiswork emphasis on analysis of the using of a flapping wing type of UAV. Wings with different shapes will be analysed andits behaviour will be studied in different air borne conditions. ANSYS CFX solver is used for the analysis purpose.
Purvi M. Joshi, “WING ANALYSIS OF A FLAPPING WING UNMANNED AERIAL VEHICLE USING CFD”, International Journal of Advance Engineering and Research Development (IJAERD), Vol. 2, Issue 5, pp. 216-221, May 2015.
