Prediction of drag coefficient of a hybrid body design of aircraft

This study presents a design of a quintessential hybrid body aircraft, a blended NACA 4414 airfoil winged body. The Design of Elements approach, via Response Surface Methodology (RSM), is used to evaluate the influence of frontal area, chamber angle and materials on the drag coefficient. The Analys...

Full description

Bibliographic Details
Main Authors: Shreya Viswanath, Riya Vasan, Venkatachalam Gopalan, Nilesh Satonkar
Format: Article
Language:English
Published: Igor Sikorsky Kyiv Polytechnic Institute 2023-12-01
Series:Mechanics and Advanced Technologies
Subjects:
Online Access:https://journal.mmi.kpi.ua/article/view/284872