Developments in computational 3-D steady aerodynamics software focusing on the efficient aerodynamic design of the next generation of transport aircraft, are surveyed. The major aerodynamic problem areas accessible to computational aerodynamics are discussed. The coherence in computational methods development is explained by showing how the methods cover a growing part of the aircraft operating range. The development of the most advanced methods, based on the Euler and Reynolds-average Navier-Stokes equations, is outlined. Computing aspects are reviewed.
Trends in Computational Fluid Dynamics (Cfd) for Aeronautical 3D Steady Applications: The Dutch Situation
1986
21 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Aircraft configurations , Aircraft design , Computational fluid dynamics , Transport aircraft , Three dimensional flow , Computer programs , Euler equations of motion , Flow geometry , Navier-stokes equation , Run time (Computers) , Steady flow , Technology assessment , User requirements , Foreign technology
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