"Design And Analysis of Aircraft Wing" by prabhat dixit Graduate Engineer, Vivek Rathod Graduate Engineer et al.

Graduate Research in Engineering and Technology (GRET)

Article Title

Authors

prabhat dixit Graduate Engineer, Department of Aerospace Engineering, SOET, Sandip University, Nashik, Maharastra, INDIAFollow
Vivek Rathod Graduate Engineer, Department of Aerospace Engineering. Sandip University, Nashik, MaharashtraFollow
Deshmukh Chetan Pravin Graduate Engineer, Department of Aerospace Engineering, SOET, Sandip University, Nashik, Maharashtra, INDIAFollow
Piyush Patil Graduate Engineer, Department of Aerospace Engineering, SOET, Sandip University, Nashik, Maharashtra, INDIAFollow

Abstract

This research develops and analyses a general aviation plane. A preliminary representation of the eventual product is used to start the design process for an airplane. Based on a drawing, a design mission profile is utilized to determine the weight. A more advanced approach is used to estimate weight, which employs calculated performance criteria to produce a more exact weight estimate. The wing design has been demonstrated to be a feasible alternative for a similar general aviation aircraft. When traveling through air or other fluids, a wing is a type of fin that provides lift. Airfoils may be observed on the wings, which have a streamlined cross-section, as a result of this. The lift created by a wing is compared to the drag generated by it to determine its aerodynamic efficiency.

Recommended Citation

dixit, prabhat Graduate Engineer; Rathod, Vivek Graduate Engineer; Pravin, Deshmukh Chetan Graduate Engineer; and Patil, Piyush Graduate Engineer (2022) "Design And Analysis of Aircraft Wing," Graduate Research in Engineering and Technology (GRET): Vol. 1: Iss. 7, Article 20.
DOI: 10.47893/GRET.2022.1133
Available at: https://www.interscience.in/gret/vol1/iss7/20

DOI

10.47893/GRET.2022.1133

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