Info
- Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.
Advances in Simulation of Wing and Nacelle Stall : 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 : 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
Continuum mechanics Aerospace engineering Astronautics Engineering Fluid Dynamics Continuum Mechanics 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 | ||
| ||
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 | ||
| ||
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 | ||
| ||
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 | ||
| ||
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 | ||
| ||
Smart Morphing and Sensing for Aeronautical Configurations : Prototypes, Experimental and Numerical Findings from the H2020 N° 723402 SMS EU Project / / edited by Marianna Braza, Jean-François Rouchon, George Tzabiras, Franco Auteri, Pawel Flaszynski
| Smart Morphing and Sensing for Aeronautical Configurations : Prototypes, Experimental and Numerical Findings from the H2020 N° 723402 SMS EU Project / / edited by Marianna Braza, Jean-François Rouchon, George Tzabiras, Franco Auteri, Pawel Flaszynski |
| Edizione | [1st ed. 2023.] |
| Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2023 |
| Descrizione fisica | 1 online resource (287 pages) |
| Disciplina |
629.1343
629.13432 |
| Collana | Notes on Numerical Fluid Mechanics and Multidisciplinary Design |
| Soggetto topico |
Fluid mechanics
Aerospace engineering Astronautics Automatic control Robotics Automation Engineering Fluid Dynamics Aerospace Technology and Astronautics Control, Robotics, Automation |
| ISBN | 3-031-22580-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Prototypes and electroactive actuators design -- Subsonic regime sRS wing -- Transonic regime tRS wing -- Sensing -- Control law definition -- Experimental study of the aerodynamic performance increase Subsonic regime -- Transonic regime -- Prototype and actuator design -- Sensing multipoint system through Bragg grating -- Control law definition -- Experimental study - characterization of the LS in take-off conditions -- Advanced CFD -- Structural mechanics involving electroactive properties -- Numerical results on the sRS prototype: take-off conditions -- Numerical results on the tRS prototype: cruise conditions -- Numerical results on the LS prototype: take-off and landing -- Sensitivity analysis through adjoined-based MDO -- Numerical results on the whole aircraft (morphing A320) -- Synthesis on the numerical simulations major outcomes -- sRS control for aerodynamic performance increase -- tRS final experimental evaluation in cruise -- LS final experimental evaluation in take-off and landing -- Synthesison the final demonstrators. |
| Record Nr. | UNINA-9910672441703321 |
| Cham : , : Springer International Publishing : , : Imprint : Springer, , 2023 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 | ||
| ||
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 | ||
| ||
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 | ||
| ||
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 | ||
| ||
