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New results in numerical and experimental fluid mechanics VIII : contributions to the 17th STAB/DGLR symposium, Berlin, Germany, 2010 / Andreas Dillman, Gerd Heller, Hans-Peter Kreplin, Wolfgang Nitsche, Inken Peltzer (eds.).

By: Dillmann, Andreas [Editor].
Contributor(s): Heller, Gerd [Editor.] | Kreplin, Hans-Peter [Editor.] | Nitsche, Wolfgang [Editor.] | Peltzer, Inken [Editor.].
Material type: TextTextSeries: Notes on numerical fluid mechanics and multidisciplinary design, Volume 121.Publisher: Heidelberg : Springer, [2013]Description: xvii, 749 páginas : ilustraciones, 25 x 17 cm.Content type: Texto ISBN: 9783642356797.Subject(s): Aviones -- Diseño y construcción Airplanes | Turbulencia | Dinámica de fluidosDDC classification: 629.1323 Online resources: Tabla de contenidos
Contents:
Investigation of the Impact of Simplifying the Aircraft Geometry on the Characteristics of the Vertical Tailplane -- Aerodynamic Optimization of a High-Lift System with Kinematic Constraints -- Simulation of Store Separation Scaling Requirements for Wind Tunnel Experiments and Validation of Numerical Simulations -- Aerodynamic Optimal Engine Integration at the Fuselage Tail of a Generic Business Jet Configuration -- Analytical Design of an Inlet Distortion Generator and Its Experimental and Numerical Validation
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Item type Current location Call number Copy number Status Date due Barcode Item holds
Libros Libros BIBLIOTECA DE ING. QUÍMICA Y AGROINDUSTRIA
629.1323/D578 (Browse shelf) Ej. 1 Available BIQA18030141
Libros Libros BIBLIOTECA DE ING. QUÍMICA Y AGROINDUSTRIA
629.1323/D578 (Browse shelf) Ej. 2 Available BIQA18030142
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Incluye referencias bibliográficas e índice

Investigation of the Impact of Simplifying the Aircraft Geometry on the Characteristics of the Vertical Tailplane -- Aerodynamic Optimization of a High-Lift System with Kinematic Constraints -- Simulation of Store Separation Scaling Requirements for Wind Tunnel Experiments and Validation of Numerical Simulations -- Aerodynamic Optimal Engine Integration at the Fuselage Tail of a Generic Business Jet Configuration -- Analytical Design of an Inlet Distortion Generator and Its Experimental and Numerical Validation

EPN Compra 01/03/2018 71019 247.50 Ej. 2

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