Following the technical program of the AGARD Fluid Dynamics Panel (FDP) for the past few years, the aeronautical engineer has found many subjects related to a special technical discipline and directed to industrial applications. But in nearly all cases the analysis of given geometry by experimental or theoretical techniques has overruled the more important engineering task, i.e., the design of a new shape which has desired properties. But in all cases concerning successful flying aircraft the result of engineering work has ben a design compromise achieved by the fruitful cooperation of all technically relevant disciplines. Therefore, one of the most important intentions of this course has been to attract people from different aeronautical disciplines, working in industry and research institutes, and to look for links within the different branches of aerodynamics such as Wind Tunnel Test Techniques, Computational Fluid Dynamics, Vortex Dynamics, Unsteady Aerodynamics, Viscous Flow Drag Prediction, and their impact on designing aircraft components.
Fundamentals of Fighter Aircraft Design
1987
5 pages
Report
Keine Angabe
Englisch
Aircraft , Aerodynamic configurations , Aeronautical engineering , Aerospace industry , Aircraft design , Fighter aircraft , Technology assessment , Computational fluid dynamics , Industries , North atlantic treaty organization (Nato) , Research facilities , Unsteady flow , Viscous drag , Viscous flow , Vortices , Wind tunnel tests , Foreign technology
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