1. N. C. AJAY VISHWATH - Assistant Professor, Department of Aeronautical Engineering, Parul Institute of Engineering and
Technology, Parul University, Vadodara, India.
2. SUJEET KUMAR PANDEY - Assistant Professor, Department of Aeronautical Engineering, Sandip University, Nashik, India.
3. PRAPTI BARAUA - UG Student, Department of Aeronautical Engineering, Parul Institute of Engineering and Technology, Parul
University, Vadodara, India.
4. POLA MANEESHWAR - UG Student, Department of Aeronautical Engineering, Parul Institute of Engineering and Technology, Parul
University, Vadodara, India.
5. DILEEP SAJJA - UG Student, Department of Aeronautical Engineering, Parul Institute of Engineering and Technology, Parul
University, Vadodara, India.
6. VAMSHI KRISHNA MUDIKE - UG Student, Department of Aeronautical Engineering, Parul Institute of Engineering and Technology, Parul
University, Vadodara, India.
This research work begins with the definition of cyclorotor and aero amphibious vehicles. The superimposition of vortex flow with non-lifting flow over a cylinder being discussed to show that such theoretical concepts could have practical application. The Design portion mentioned in this manuscript deals with every design aspect from the dimensions to the various Dynamic forces acting on the Aeroamphibious Cyclorotor body. Motor directions with high or low logic puts this manuscript to a programming domain, still the extensive calculations involved with the lift and drag equations for each rotor blades and the overall lift with motor RPM brings it to a descent aerodynamic domain. The extensive calculations involve in this research work includes both aerial conditions as well as aquatic conditions.
PROBLEMS ASSOCIATED WITH THE STABILITY OF BICOPTERS AND TRICOPTERS.