11 Page 11-22 © MANTECH PUBLICATIONS 2021. All Rights Reserved International Journal of Mechatronics and Manufacturing Technology Volume 6 Issue 1 Conceptual Design of Multi-Cambered Bioinspired Morphing Wing K Madhulaalasa 1* , D Divya Govind 2 , M Manoj Kumar 3 , Y D Dwivedi 4 UG Student 1, 2, 3 , Professor 4 Department of Aeronautical Engineering Institute of Aeronautical Engineering, Hyderabad, India-500043 Corresponding AuthorsEmail id: janukurma00@gmail.com 1* , divyagovind134@gmail.com 2 , manojmalluri.1999@gmail.com 3 , yddwivedi@gmail.com 4 Abstract The idea of air transportation has been inspired by birds, but the present advanced aeronautical technology could not mimic the complete flight performance of the birds. The objective of this paper is to design the structure of bird wing conceptually by using variable camber along the length of the wing to reach the artificial requirement of the bird performance. Since each different way will result in unique flight performance, the multi cambered section configuration in the wing is chosen and studied. Such a wing might enhance the flying capabilities through flapping. The complexity of creating the bird's wing is studied. Instead of providing the changing shape in the wings to achieve its flight, the multi-camber wing will be designed and drafted in Catia V5, in which the camber and airfoil will be different along its length. This conceptual design will create a wing without intruding on its structure. Moreover, the flight ability of birds is not completely dependent on its morphing design of wing but also on discrete wing structure having feathers and winglets. Keywords: - Multi-cambered, bird flight, morphing, flapping. INTRODUCTION One of the oldest dreams of aeronautical engineers is to fly like a bird, and the studies were based on the fascinating performance of birds‟ flight, which always mesmerized the researchers thought in trying to replicate the same. Early attempts to recreate the aerodynamics of bird wing without understanding the principles behind resulted in failure. However, after