New Results in Numerical and Experimental Fluid Mechanics IV, 2004 Contributions to the 13th STAB/DGLR Symposium Munich, Germany 2002 Notes on Numerical Fluid Mechanics and Multidisciplinary Design Series, Vol. 87
Langue : Anglais
This volume contains 59 papers presented at the 13th Symposium of STAB (German Aerospace Aerodynamics Association). In this association, all those German scientists and engineers from universities, research establishments and industry are involved who are doing research and project work in numerical and experimental fluid mechanics and aerodynamics, mainly for aerospace but also in other applications. Many of the contributions give results from federal and European-Union sponsored projects. The volume gives a broad overview of the ongoing work in this field in Germany. Covered are flow problems of high and low aspect-ratio wings and bluff bodies, laminar flow control and transition, hypersonic flows, transition and fluid mechanical modelling, LES and DNS, numerical simulation, aeroelasticity, measuring techniques and propulsion flows.
High Aspect-Ratio Wings: Wake Vortex and Configurations.- High-Lift.- Engine-Integration.- Numerical Simulation.- Low Aspect-Ratio Wings.- Bluff Bodies.- Laminar Flow Control and Transition.- Hypersonic Flows: Design and Configurations.- Facilities and Measuring Techniques.- Propulsion and Facilities.- Aeroelasticity.- Transition and Fluidmechanical Modelling.- Fluidmechanical Modelling; Numerical Modelling: LES and DNS.- Numerical Simulation: Mathematical Fundamentals.- Grid Generation and Flow Solvers.- Measuring Techniques.- Propulsion.
Broad overview about ongoing work and results in Aerospace in Germany Collected results of project work in numerical and experimental aerodynamics and fluidmechanics for aerospace and other applications Includes supplementary material: sn.pub/extras
Date de parution : 08-2012
Ouvrage de 484 p.
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Ajouter au panierDate de parution : 01-2004
Ouvrage de 484 p.
Thèmes de New Results in Numerical and Experimental Fluid Mechanics IV :
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