Configuration optimization, component design, and experimental proof in fighter design are summarized. Requirements for supersonic performance, including supersonic drag reduction and canard tail design, were reviewed. The main aerodynamic principles in use throughout the aircraft industry are described.
Computational Aerodynamic Design Tools and Techniques Used at Fighter Development
1979
54 pages
Report
Keine Angabe
Englisch
Optimization , Foreign technology , Aircraft industry , Aerodynamics , Aircraft , Aircraft structures , Aircraft design , Canard configurations , Supersonic flight , Aircraft configurations , Structural design , Aeronautical engineering , Control surfaces , Drag reduction , Fighter aircraft , Supersonic flow , Aerodynamic configurations
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