ADDITIONAL MENU
- Reviewer Team
- Focus & Scope
- Section Policies
- Publication Frequency
- Peer Review Process
- Publication Ethics
- Copyright & License
- Plagiarism Policy
- Author Guidelines
- Visitor Statistics
Download
Visitor Statistics
In this research, analysis of loads model was taken to determine critical design loads of components of the aircraft in order to find out the balance loads of the total body of still developing IFX fighter aircraft. Analysis of aircraft’s loads was taken to determine the required strength of the IFX structure. The result of research and development of IFX fighter aircraft so far shows that its loads model needs to be complemented by CFD study and wind tunnel test.