This volume collects contributions to the 14th Symposium of the STAB (German Aerospace Aerodynamics Association). The association involves German scientists and engineers from universities, research establishments and industry who are doing research and project work in numerical and experimental fluid mechanics and aerodynamics, mainly for aerospace but for other applications, too. The volume gives a broad overview of ongoing work in Germany in this field.
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This volume contains the contributions to the 14. Symposium of the 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 for other applications, too. Many of the contributions are presenting results from national and European Community sponsored projects. The volume gives a broad overview over the ongoing work in this field in Germany, with the topics being high-aspect ratio wings, low aspect-ratio wings, bluff bodies, laminar flow control and transition, active flow control, hypersonic flows, aeroelasticity, aeroacoustics, mathematical fundamentals/ numerical simulation, physical fundamentals, and facilities.
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plasma actuators, transition prediction module, deflected leading edge, unsteady air loads, free stream consistency, laminar wing glove, numerical rebuilding, viscous core radius, wing tip devices, active separation control, deformation measurement technique, jet pressure ratio, research airfoil, trailing edge noise, central solver, delta wing flow, flap vortex, transonic dip, noise reduction potential, trapezoid wing, edge noise reduction, stall behaviour, laminar separation points, transitional flow regions, whirl flux Key Phrases - Capitalized Phrases (CAPs): (learn more)
Fluid Mech, Reynolds-averaged Navier-Stokes, Springer Verlag, German Aerospace Center, Technical Report, Navier Stokes, Technische Universität Munchen, New York, Universität Stuttgart, Airbus Deutschland, Computational Physics, Deutsches Zentrum, European Union, International Conference, Braunschweig Technical University, Calculation of Complex, Deutsche Forschungsgemeinschaft, Journal of Aircraft, Stuttgart University, Technische Universität München, The Netherlands, Aeroacoustic Wind Tunnel Braunschweig, Bienroder Weg, Dresden University of Technology, Eurocopter Deutschland New!
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plasma actuators, transition prediction module, deflected leading edge, unsteady air loads, free stream consistency, laminar wing glove, numerical rebuilding, viscous core radius, wing tip devices, active separation control, deformation measurement technique, jet pressure ratio, research airfoil, trailing edge noise, central solver, delta wing flow, flap vortex, transonic dip, noise reduction potential, trapezoid wing, edge noise reduction, stall behaviour, laminar separation points, transitional flow regions, whirl flux Key Phrases - Capitalized Phrases (CAPs): (learn more)
Fluid Mech, Reynolds-averaged Navier-Stokes, Springer Verlag, German Aerospace Center, Technical Report, Navier Stokes, Technische Universität Munchen, New York, Universität Stuttgart, Airbus Deutschland, Computational Physics, Deutsches Zentrum, European Union, International Conference, Braunschweig Technical University, Calculation of Complex, Deutsche Forschungsgemeinschaft, Journal of Aircraft, Stuttgart University, Technische Universität München, The Netherlands, Aeroacoustic Wind Tunnel Braunschweig, Bienroder Weg, Dresden University of Technology, Eurocopter Deutschland New!
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Front Cover | Table of Contents | First Pages | Back Cover | Surprise Me!
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