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Advances in Simulation of Wing and Nacelle Stall [[electronic resource] ] : Results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany / / edited by Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends
Advances in Simulation of Wing and Nacelle Stall [[electronic resource] ] : Results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany / / edited by Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends
Edizione [1st ed. 2016.]
Pubbl/distr/stampa Cham : , : Springer International Publishing : , : Imprint : Springer, , 2016
Descrizione fisica 1 online resource (404 p.)
Disciplina 629.13432
Collana Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Soggetto topico Fluid mechanics
Fluids
Aerospace engineering
Astronautics
Engineering Fluid Dynamics
Fluid- and Aerodynamics
Aerospace Technology and Astronautics
ISBN 3-319-21127-7
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto The Delay of RANS-to-LES Transition in Hybrid RANS-LES Approaches and Some Recently Proposed Remedies -- Computations of Separated Flows with a Hybrid RANS/LES Approach -- Hybrid RANS/LES Study of the Development of an Airfoil-Generated Vortex -- Interaction of Three-Dimensional Disturbances with the Flow around a Two-Element High-Lift Airfoil -- The Discontinuous Galerkin Method as an Enabling Technology for DNS and LES of Industrial Aeronautical Applications -- Body Force Modelling of Internal Geometry for Jet Noise Prediction -- Numerical Studies of Turbulent Flow Influence on a Two-Element Airfoil -- CFD for Prediction of Flow Separation from Aircraft Tail Surfaces -- Zonal RANS-LES Computation for Near-Stall-Airfoil Flow -- Criteria for Crosswind Variations during Approach and Touchdown at Airports -- Development and Improvement of Two Methods of Different Complexity to Simulate Atmospheric Boundary Layer Turbulence for Aircraft Design Studies -- Simulation of Interaction of Aircraft with Gust and Resolved LES-Simulated Atmospheric Turbulence -- A New Method to Generate Anisotropic Synthetic Turbulence for LES -- Numerical Simulation of the Turbulent Flow Around a Wing -- Integration- and Intake-Induced Flow Distortions and their Impact on Aerodynamic Fan Performance -- Flow Investigations in a Stalling Nacelle Inlet Under Disturbed Inflow -- Realistic Inlet Distortion Patterns Interacting with a Transonic Compressor Stage -- Unsteady CFD Simulation of Transonic Axial Compressor Stages with Distorted Inflow -- Transitional Shock-Wave/Boundary-Layer Interactions in Intakes at Incidence.-Advanced Design Approach for a High-lift Wind Tunnel Model Based on Flight Test Data -- Simulation of Longitudinal Vortices on a High-LiftWing -- Impact of Different UHBR-Engine Positions on the Aerodynamics of a High-LiftWing -- Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration -- Numerical Studies of Active Flow Control Applied at the Engine-Wing Junction.
Record Nr. UNINA-9910254190203321
Cham : , : Springer International Publishing : , : Imprint : Springer, , 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Aerofoil sections : results from wind-tunnel investigations, theoretical foundations / by Friedrich Wilhelm Riegels ; translated from the German by D. G. Randall
Aerofoil sections : results from wind-tunnel investigations, theoretical foundations / by Friedrich Wilhelm Riegels ; translated from the German by D. G. Randall
Autore Riegels, Friedrich Wilhelm
Pubbl/distr/stampa London : Butterworths, 1961
Descrizione fisica 281 p. : ill. ; 29 cm
Disciplina 629.13432
Soggetto non controllato Aerodinamica
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-990008443990403321
Riegels, Friedrich Wilhelm  
London : Butterworths, 1961
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Boundary layer and flow control : its principles and application / edited by G. V. Lachmann
Boundary layer and flow control : its principles and application / edited by G. V. Lachmann
Pubbl/distr/stampa Oxford [etc.] : Pergamon Press, 1961
Descrizione fisica v. : ill. ; 24 cm
Disciplina 629.13432
Soggetto non controllato Dinamica dei fluidi
Strato di contorno - Aerodinamica
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto 1. - XII, 600 p. 2. - VI, P. 603-1360
Record Nr. UNINA-990008443280403321
Oxford [etc.] : Pergamon Press, 1961
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Ice accretion and icing technology / / Robert J. Flemming
Ice accretion and icing technology / / Robert J. Flemming
Autore Flemming Robert J.
Pubbl/distr/stampa Warrendale, Pa. (400 Commonwealth Dr., Wallendale PA USA) : , : Society of Automotive Engineers, , 2015
Descrizione fisica 1 online resource (xii, 107 pages) : illustrations
Disciplina 629.13432
Collana Society of Automotive Engineers. Electronic publications
Soggetto topico Airplanes - Ice prevention
Aeronautics - Safety meaures
Airplanes - Climatic factors
ISBN 0-7680-8713-9
0-7680-8189-0
1-5231-0224-1
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Introduction -- Effect of stagnation flow on an impacting water droplet on a superhydrophobic surface (2013-01-2174) -- Icing process of supercooled-water droplet moving on a surface by using luminescent temperature-imaging technique (2013-01-2210) -- Considerations on the use of hydrophobic, superhydrophobic or icephobic coatings as a part of the aircraft ice protection system (2013-01-2108) -- Evaluation of icing scaling on swept NACA 0012 airfoil models (2011-38-0081) -- New SLD icing capabilities at DGA aero-engine testing (2011-38-0086) -- S-76D tail rotor ice impact test (2011-38-0101) -- Numerical correlation between meteorological parameters and aerodynamic performance degradation of iced airfoils (2013-01-2137) -- Calculation of ice shapes on oscillating airfoils (2011-38-0015) -- Oscillating airfoil icing tests in the NASA Glenn Research Center Icing Research Tunnel (2011-38-0016) -- In-flight icing of UAVs - The influence of Reynolds Number on the ice accretion process (2011-01-2572) -- About the editor.
Record Nr. UNINA-9910438322303321
Flemming Robert J.  
Warrendale, Pa. (400 Commonwealth Dr., Wallendale PA USA) : , : Society of Automotive Engineers, , 2015
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Modern flexible multi-body dynamics modeling methodology for flapping wing vehicles / / Cornelia Altenbuchner, James E. Hubbard, Jr
Modern flexible multi-body dynamics modeling methodology for flapping wing vehicles / / Cornelia Altenbuchner, James E. Hubbard, Jr
Autore Altenbuchner Cornelia
Pubbl/distr/stampa London, England : , : Academic Press, , 2018
Descrizione fisica 1 online resource (200 pages) : illustrations (some color), tables, graphs, photographs
Disciplina 629.13432
Soggetto topico Airplanes - Wings
Aerospace engineering - Computer simulation
Wings (Anatomy) - Aerodynamics
ISBN 0-12-814137-9
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910583454503321
Altenbuchner Cornelia  
London, England : , : Academic Press, , 2018
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Theory of wing sections : including a summary of Airfoil data / by Ira H. Abbott, A. E. Von Doenhoff
Theory of wing sections : including a summary of Airfoil data / by Ira H. Abbott, A. E. Von Doenhoff
Autore ABBOTT, Ira H.
Pubbl/distr/stampa New York [etc.] : Dover, 1980
Descrizione fisica 703 p. ; 21 cm
Disciplina 629.13432
Altri autori (Persone) DOENHOFF, Albert E. : von
Soggetto topico Ingegneria aeronautica
Aeromobili - Costruzione
ISBN 0-486-60586-8
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNISA-990002409870203316
ABBOTT, Ira H.  
New York [etc.] : Dover, 1980
Materiale a stampa
Lo trovi qui: Univ. di Salerno
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Theory of wing sections : including a summary of airfoil data / by Ira H. Abbott, Albert E. von Doenhoff
Theory of wing sections : including a summary of airfoil data / by Ira H. Abbott, Albert E. von Doenhoff
Autore Abbott, Ira H.
Pubbl/distr/stampa New York : Dover, copyr. 1959
Descrizione fisica X, 693 p. ; 22 cm
Disciplina 629.13432
Collana Dover books on engineering and engineering physics
Soggetto non controllato Aerodinamica
Profili
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-990000534870403321
Abbott, Ira H.  
New York : Dover, copyr. 1959
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Theory of wing sections : including a summary of airfoil data / Ira H. Abbott, Albert E. Von Doenhoff
Theory of wing sections : including a summary of airfoil data / Ira H. Abbott, Albert E. Von Doenhoff
Autore Abbott, Ira H.
Edizione [Nuova ed]
Pubbl/distr/stampa New York : Dover, 1959
Descrizione fisica X, 693 p. : ill. ; 22 cm.
Disciplina 629.13432
Altri autori (Persone) Von Doenhoff, Albert Edward
ISBN 04-86605-86-8
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNICAMPANIA-SUN0035675
Abbott, Ira H.  
New York : Dover, 1959
Materiale a stampa
Lo trovi qui: Univ. Vanvitelli
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Theory of wing sections : including a summary of airfoil data / Ira H. Abbott, Albert E. Von Doenhoff
Theory of wing sections : including a summary of airfoil data / Ira H. Abbott, Albert E. Von Doenhoff
Autore Abbott, Ira H.
Edizione [Nuova ed]
Pubbl/distr/stampa New York, : Dover, 1959
Descrizione fisica X, 693 p. : ill. ; 22 cm
Disciplina 629.13432
Altri autori (Persone) Von Doenhoff, Albert Edward
ISBN 04-86605-86-8
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Titolo uniforme
Record Nr. UNICAMPANIA-VAN0035675
Abbott, Ira H.  
New York, : Dover, 1959
Materiale a stampa
Lo trovi qui: Univ. Vanvitelli
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Theory of wing sections, including a summary of airfoil data, by Ira H. Abbott and Albert E. von Doenhoff
Theory of wing sections, including a summary of airfoil data, by Ira H. Abbott and Albert E. von Doenhoff
Autore Abbott, Ira Herbert, 1906-
Edizione [[Corr. version, with a new pref. by the authors]]
Pubbl/distr/stampa New York, Dover Publicationsc1959
Descrizione fisica 693 p. : ill. ; 22 cm
Disciplina 629.13432
Altri autori (Persone) Doenhoff, Albert E. von (Albert Edward), 1910
Soggetto topico Airplanes - Wings
Aerodynamics
Aerofoils
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNISALENTO-991001430329707536
Abbott, Ira Herbert, 1906-  
New York, Dover Publicationsc1959
Materiale a stampa
Lo trovi qui: Univ. del Salento
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