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...
Saved in:
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
National Technical University of Ukraine "Igor Sikorsky Kyiv Polytechnic Institute"
2023-12-01
|
| Series: | Mechanics and Advanced Technologies |
| Subjects: | |
| Online Access: | https://journal.mmi.kpi.ua/article/view/284872 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|