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...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
Published: |
Igor Sikorsky Kyiv Polytechnic Institute
2023-12-01
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Series: | Mechanics and Advanced Technologies |
Subjects: | |
Online Access: | https://journal.mmi.kpi.ua/article/view/284872 |