Modern aerodynamic methods for direct and inverse applications / / Wilson C. Chin |
Autore | Chin Wilson C. |
Pubbl/distr/stampa | Hoboken, NJ : , : Wiley, , [2019] |
Descrizione fisica | 1 online resource (439 pages) |
Disciplina | 629.1323 |
Collana | THEi Wiley ebooks |
Soggetto topico | Aerodynamics |
ISBN |
1-119-58086-2
1-119-58122-2 1-119-58085-4 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910555072803321 |
Chin Wilson C.
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Hoboken, NJ : , : Wiley, , [2019] | ||
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Lo trovi qui: Univ. Federico II | ||
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Modern aerodynamic methods for direct and inverse applications / / Wilson C. Chin |
Autore | Chin Wilson C. |
Pubbl/distr/stampa | Hoboken, NJ : , : Wiley, , [2019] |
Descrizione fisica | 1 online resource (439 pages) |
Disciplina | 629.1323 |
Collana | THEi Wiley ebooks |
Soggetto topico | Aerodynamics |
ISBN |
1-119-58086-2
1-119-58122-2 1-119-58085-4 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910811097803321 |
Chin Wilson C.
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Hoboken, NJ : , : Wiley, , [2019] | ||
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Lo trovi qui: Univ. Federico II | ||
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Modern compressible flow : with historical perspective / John D. Anderson, Jr. |
Autore | Anderson, John David |
Edizione | [3rd.ed] |
Pubbl/distr/stampa | Boston : McGraw-Hill, 2004 |
Descrizione fisica | XVI, 760 p. : ill. ; 23 cm |
Disciplina | 629.1323 |
Soggetto non controllato |
Volo meccanico - Dinamica
Aeroplani - Dinamica |
ISBN | 007-124136-1 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-990008542750403321 |
Anderson, John David
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Boston : McGraw-Hill, 2004 | ||
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Lo trovi qui: Univ. Federico II | ||
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New Results in Numerical and Experimental Fluid Mechanics IX : Contributions to the 18th STAB/DGLR Symposium, Stuttgart, Germany, 2012 / / edited by Andreas Dillmann, Gerd Heller, Ewald Krämer, Hans-Peter Kreplin, Wolfgang Nitsche, Ulrich Rist |
Edizione | [1st ed. 2014.] |
Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2014 |
Descrizione fisica | 1 online resource (640 p.) |
Disciplina | 629.1323 |
Collana | Notes on Numerical Fluid Mechanics and Multidisciplinary Design |
Soggetto topico |
Fluid mechanics
Physics Aerospace engineering Astronautics Fluids Engineering Fluid Dynamics Numerical and Computational Physics, Simulation Aerospace Technology and Astronautics Fluid- and Aerodynamics |
ISBN | 3-319-03158-9 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Airplane Aerodynamics -- Optimization -- Laminar Flow Control and Transition -- Rotorcraft Aerodynamics -- Convective Flows -- Aerodynamics and Aeroacoustics of Ground Vehicles -- Aeroelasticity and Structural Dynamics -- Numerical Simulation -- Experimental Simulation and Test Techniques -- Aeroacoustics -- Biofluid Mechanics. |
Record Nr. | UNINA-9910299484703321 |
Cham : , : Springer International Publishing : , : Imprint : Springer, , 2014 | ||
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Lo trovi qui: Univ. Federico II | ||
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New Results in Numerical and Experimental Fluid Mechanics X : Contributions to the 19th STAB/DGLR Symposium Munich, Germany, 2014 / / edited by Andreas Dillmann, Gerd Heller, Ewald Krämer, Claus Wagner, Christian Breitsamter |
Edizione | [1st ed. 2016.] |
Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2016 |
Descrizione fisica | 1 online resource (855 p.) |
Disciplina | 629.1323 |
Collana | Notes on Numerical Fluid Mechanics and Multidisciplinary Design |
Soggetto topico |
Fluid mechanics
Continuum mechanics Aerospace engineering Astronautics Transportation engineering Traffic engineering Engineering Fluid Dynamics Continuum Mechanics Aerospace Technology and Astronautics Transportation Technology and Traffic Engineering |
ISBN | 3-319-27279-9 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Part I Airplane Aerodynamics / Propulsion Integration -- Part II Optimization -- Part III Turbulence Research and Turbulence Modeling -- Part IV Laminar Flow Control and Transition -- Part V Rotorcraft Aerodynamics -- Part VI Technical Flows -- Part VII Vehicle Aerodynamics -- Part VIII Aeroelasticity and Structural Dynamics -- Part IX Numerical Simulation / Aerodynamics -- Part X Experimental Aerodynamics / Experimental Simulation and Test Techniques -- Part XI Aeroacoustics -- Part XII Hypersonic Aerodynamics -- Part XIV Wind Energy. . |
Record Nr. | UNINA-9910254256203321 |
Cham : , : Springer International Publishing : , : Imprint : Springer, , 2016 | ||
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Lo trovi qui: Univ. Federico II | ||
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New Results in Numerical and Experimental Fluid Mechanics XI : Contributions to the 20th STAB/DGLR Symposium Braunschweig, Germany, 2016 / / edited by Andreas Dillmann, Gerd Heller, Ewald Krämer, Claus Wagner, Stephan Bansmer, Rolf Radespiel, Richard Semaan |
Edizione | [1st ed. 2018.] |
Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2018 |
Descrizione fisica | 1 online resource (XV, 767 p. 465 illus., 360 illus. in color.) |
Disciplina | 629.1323 |
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 | 3-319-64519-6 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | PART I: New Results in Numerical and Experimental Fluid Mechanics XI -- PART II: Turbulence Research and Turbulence Modeling -- PART III: Hypersonic Aerodynamics -- PART IV: Laminar Flow Control and Transition -- PART V: High-Agility Configuration -- PART VI: Rotorcraft Aerodynamics -- PART VII: Aeroelasticity and Structural Dynamics -- PART VIII: Numerical Simulation/Aerodynamics -- PART IX: Experimental Aerodynamics/Experimental Simulation and Test Techniques -- PART X: Aeroacoustics -- PART XI: Vehicle Aerodynamics -- PART XII: Wind Energy. |
Record Nr. | UNINA-9910299874703321 |
Cham : , : Springer International Publishing : , : Imprint : Springer, , 2018 | ||
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Lo trovi qui: Univ. Federico II | ||
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New Results in Numerical and Experimental Fluid Mechanics XIII : Contributions to the 22nd STAB/DGLR Symposium / / edited by Andreas Dillmann, Gerd Heller, Ewald Krämer, Claus Wagner |
Edizione | [1st ed. 2021.] |
Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2021 |
Descrizione fisica | 1 online resource (788 pages) : illustrations (chiefly color) |
Disciplina | 629.1323 |
Collana | Notes on Numerical Fluid Mechanics and Multidisciplinary Design |
Soggetto topico |
Fluid mechanics
Aerospace engineering Astronautics Continuum mechanics Engineering Fluid Dynamics Aerospace Technology and Astronautics Continuum Mechanics |
ISBN | 3-030-79561-6 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Influence of the Wind Tunnel Model Mounting on the Wake Evolution of the Common Research Model in Post Stall -- Assessment of the Disturbance Velocity Approach to Determine the Gust Impact on Airfoils in Transonic Flow -- Comparison of Different Methods for the Extraction of Airfoil Characteristics of Propeller Blades as Input for Propeller Models in CFD -- Stochastic Modeling of Passive Scalars in Turbulent Channel Flows: Predictive Capabilities of One-Dimensional Turbulence -- Study on Large-Scale Amplitude Modulation of Near-Wall Small-Scale Structures in Turbulent Wall-Bounded Flows -- Investigation of Coherent Motions in a Flat-Plate Turbulent Boundary Layer with Adverse Pressure Gradient -- Experimental Approach on Concentration Measurements of NO in Hydrogen Combustion based on Heterodyne Laser Absorption Spectroscopy using Quantum Cascade Lasers -- Internal Application of Ultra-Fast Temperature Sensitive Paint to Hydrogen Combustion Flow -- Influence of Surface Irregularities on the Expected Boundary-Layer Transition Location on Hybrid Laminar Flow Control Wings. |
Record Nr. | UNINA-9910492147503321 |
Cham : , : Springer International Publishing : , : Imprint : Springer, , 2021 | ||
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Lo trovi qui: Univ. Federico II | ||
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Noise resistance enhancement in aircraft navigation and connected systems / / Dmitry Alexandrovich Zatuchny [and four others] |
Autore | Zatuchny Dmitry Alexandrovich |
Pubbl/distr/stampa | Gateway East, Singapore : , : Springer, , [2021] |
Descrizione fisica | 1 online resource (ix, 180 pages) : illustrations |
Disciplina | 629.1323 |
Collana | Springer Aerospace Technology |
Soggetto topico | Airplanes - Noise |
ISBN | 981-16-0630-7 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910484596703321 |
Zatuchny Dmitry Alexandrovich
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Gateway East, Singapore : , : Springer, , [2021] | ||
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Lo trovi qui: Univ. Federico II | ||
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Noise Sources in Turbulent Shear Flows: Fundamentals and Applications / / edited by Roberto Camussi |
Edizione | [1st ed. 2013.] |
Pubbl/distr/stampa | Vienna : , : Springer Vienna : , : Imprint : Springer, , 2013 |
Descrizione fisica | 1 online resource (452 p.) |
Disciplina | 629.1323 |
Collana | CISM International Centre for Mechanical Sciences, Courses and Lectures |
Soggetto topico |
Fluid mechanics
Aerospace engineering Astronautics Vibration Dynamical systems Dynamics Engineering Fluid Dynamics Aerospace Technology and Astronautics Vibration, Dynamical Systems, Control |
ISBN |
1-299-33778-3
3-7091-1458-6 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Fundamentals: Introduction to aero acoustics and self-sustained oscillations of internal flows -- Sound radiation by moving surfaces and the Greens functions techniques -- Applications: Jet noise -- Analysis techniques for aero acoustics: noise source identification -- Broadband noise from lifting surfaces: analytical modeling and experimental validation -- Boundary layer noise: generation mechanisms -- Interior noise radiation and control. |
Record Nr. | UNINA-9910437922503321 |
Vienna : , : Springer Vienna : , : Imprint : Springer, , 2013 | ||
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Lo trovi qui: Univ. Federico II | ||
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The proceedings of the 2021 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2021) . Volume 1 / / Sangchul Lee [and four others], editors |
Pubbl/distr/stampa | Gateway East, Singapore : , : Springer, , [2023] |
Descrizione fisica | 1 online resource (1027 pages) |
Disciplina | 629.1323 |
Collana | Lecture notes in electrical engineering |
Soggetto topico |
Aerodynamics
Aeronautics Aerospace engineering - Technological innovations |
ISBN | 981-19-2689-1 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Intro -- About APISAT 2021 -- Organization -- Contents -- Editor Bios -- Aerodynamics and Design -- Asia-Pacific Region's Aircraft Design and Development Strategy for Single-Aisle Aircraft in the Oligopoly Market of Boeing and Airbus -- 1 Introduction -- 2 Commercial Aircraft International Joint Development (IJD) -- 2.1 Demand and Supply Imbalance by Region -- 2.2 Aircraft Production of AP Countries -- 3 RSP Stage 2: Japan Success -- 3.1 Target Achievement Time of AP RSP Stage 2 -- 3.2 Japan Success Factors -- 3.3 Government, Airlines, and Manufacturers -- 4 RSP Stage 3: Europe Success Case -- 4.1 Airbus Success Factors -- 4.2 Aerospace Production Value -- 4.3 The International Joint Development Effect of SAA -- 4.4 RSP Revenue Forecast in AP -- 4.5 Long-Term Outlook on AADC -- 5 Conclusions -- References -- Study on Wind Resistance Characteristics of Multi-rotor UAV -- 1 Fire Fighting UAV Flight Platform -- 2 Analysis of Anti-wind Characteristics -- 2.1 Forward and Incoming Flow Analysis -- 2.2 Analysis of Lateral Incoming Flow -- 3 Wind Resistance Evaluation Results -- 3.1 Forward and Incoming Flow -- 3.2 Lateral Incoming Flow -- 4 Analysis Process of Wind Resistance Characteristics -- 5 Summary -- References -- Inverse Design Method of Transonic Airfoil Based on Deep Neural Network -- 1 Introduction -- 2 Modeling Method -- 2.1 Numerical Calculation Method -- 2.2 Airfoil Parameterization Method -- 2.3 Neural Network Model -- 3 Numerical Examples and Analysis -- 3.1 Training Set Establishment -- 3.2 Model Training -- 3.3 Analysis of Training Results -- 3.4 Neural Network Hyperparametric Analysis -- 4 Conclusion -- References -- High-Rise Building Wind Field Simulation -- 1 Introduction -- 2 Computational Fluid Dynamics Theory -- 2.1 Wind Field Theory -- 2.2 Fluid Mechanics Control Equation -- 3 CFD Simulation of High-Rise Building Wind Field.
3.1 Computational Domain Setting and Meshing -- 3.2 Result Analysis and Processing -- 3.3 Study on the Interference Effect of Two Buildings -- 3.4 Enclosed Layout -- 4 Conclusion -- References -- Study on Aerodynamic Characteristics of "Propeller/Wing" System with Overset Mesh Method -- 1 Introduction -- 2 Computational Strategy -- 2.1 3D Models -- 2.2 Actuator-Disk Models -- 3 Results -- 3.1 Single Propeller -- 3.2 Propeller/Wing -- 4 Conclusions -- References -- An Ontology Based Single Source of Truth (SSOT) Construction Approach for Aircraft Modeling and Simulation -- 1 Introduction -- 2 An Ontology Based SSOT Construction Approach -- 2.1 A Reference Ontology for Aircraft -- 2.2 Construct SSOT Based on Ontology -- 3 Model Transformation with Ontology Based SSOT -- 3.1 Behavior Model Transformation Example -- 3.2 Structural Model Transformation Example -- 4 Conclusion -- 5 Discussion -- References -- Experimental Investigations on Aerodynamic and Psychoacoustic Characteristics of Loop-Type Propeller -- 1 Introduction -- 2 Experiment Setup -- 2.1 Thrust and Torque Measurement -- 2.2 Sound Signal Measurement -- 2.3 Model Setup -- 3 Result -- 3.1 Aerodynamic Performance -- 3.2 Acoustic Performance -- 3.3 Objective Psychoacoustic Metrics -- 4 Discussion -- 5 Conclusion and Future Work -- References -- Effect of Dynamic Micro Vortex Generator on Corner Shock Wave Boundary Layer Interactions Based on DES -- 1 Introduction -- 2 Numerical Simulations -- 2.1 Numerical Method -- 2.2 Computational Domain Model -- 2.3 Mesh and Boundary Conditions -- 3 Verification of Numerical Methods -- 3.1 Mesh Independence -- 3.2 Numerical Simulation Accuracy -- 4 Results and Analysis -- 4.1 The Impact of Dynamic MVG on SWBLI Area Pressure -- 4.2 The Impact of Dynamic MVG on the Boundary Layer of the SWBLI Region -- 4.3 Control Mechanism of Dynamic MVG on SWBLI. 5 Conclusions -- References -- Aerodynamic Characteristics of A Compound Deflected LEF/TEF Rotor -- 1 Introduction -- 2 Numerical Method -- 2.1 Grid Generation Method -- 2.2 Aerodynamic Analysis Method -- 3 Results and Discussion -- 3.1 Aerodynamic Characteristics of an Airfoil with the LEF/TEF -- 3.2 Aerodynamic Characteristics of a Rotor with a LEF/TEF When Hovering -- 4 Conclusion -- References -- Analysis of Aerodynamic Characteristics and Influence of Parameters of the Quad Tiltrotor Aircraft -- 1 Introduction -- 2 Numerical Method -- 2.1 Geometric Model and Grid Generation -- 2.2 Calculation Method -- 2.3 Verification of the Method -- 3 Results and Analysis -- 3.1 Interferences on the Rear Rotor -- 3.2 Influence of the Rotor Rotation Direction -- 3.3 Influence of the Wing Installation Angle -- 3.4 Influence of the Rotor Transverse Distance -- 3.5 Influence of the Rotor Longitudinal Distance -- 4 Conclusions -- References -- A Two-Step Optimization Method Using POD-Based Geometric Parameterization for Aerodynamic Shape Optimization -- 1 Introduction -- 2 POD-Based Geometric Parameterization and Its Characteristics -- 2.1 Principle of POD -- 2.2 POD-Based Geometric Parameterization -- 2.3 Merits and Drawbacks -- 3 Two-Step Optimization Method for ASO -- 4 Validation Case of Rotor 37 -- 4.1 The 1st-Step Optimization -- 4.2 SD Selection and POD-Based Geometric Parameterization -- 4.3 The 2nd-Step Optimization -- 5 Conclusions -- References -- Anti-icing Performance of Engine Inlet Cone by Hot Air Film -- 1 Introduction -- 2 Numerical Investigations -- 2.1 Model and Methods -- 2.2 Boundary Conditions -- 2.3 Results and Discussions -- 3 Experimental Investigations -- 3.1 Experiment Systems -- 3.2 Experimental Results and Discussions -- 4 Conclusions -- References -- Aerodynamic Characteristics of Close UAV Formation -- 1 Introduction. 1.1 Previous Work -- 1.2 Our Work -- 2 Basic Method and Validation -- 2.1 Vortex Model -- 2.2 Nonlinear Lifting Line Theory -- 2.3 Trailing Vortex Model -- 3 Nonlinear Aerodynamic Characteristics of Wake Surfing -- 4 Conclusion -- References -- Conceptual Design and System Level Analysis of Tilt-Duct eVTOL Aircraft -- 1 Introduction -- 2 Design Requirements and Assumptions -- 2.1 Design Requirements -- 2.2 Design Assumptions -- 3 Methods -- 4 Results -- 5 Conclusion -- References -- Research on Wind Tunnel Test of the Total Pressure Probe Layout for Civil Aircraft -- 1 Introduction -- 2 Test Model -- 3 Miniature Probe -- 3.1 Seven-Hole Probe -- 3.2 Miniature Total Pressure Probe -- 4 Analysis of Test Results -- 4.1 Results of the Seven-Hole Probe -- 4.2 Results of Miniature Total Pressure Probe -- 5 Conclusion -- References -- Study on the Dynamic Aerodynamic Performance of Airfoil with Direct Force Measurement -- 1 Introduction -- 2 Descriptions of Experiments -- 2.1 Experimental Equipment and Instruments -- 2.2 Experimental Model -- 3 Elimination Method of Inertial Force and Pitching Moment -- 3.1 Elimination of Inertial Pitching Moment -- 3.2 Elimination of Inertial Force -- 4 Data Processing and Analyses -- 4.1 Data Filtering and Averaging Processing -- 4.2 Calculation of the First and Second Derivatives of the Angle of Attack with Respect to Time -- 5 Result Analyses -- 5.1 The Impact of Reduced Frequency -- 5.2 Influence of Amplitude -- 5.3 Influence of Reynolds Number -- 5.4 Effect of Average Angle of Attack -- 6 Conclusions -- References -- The Research of Correlationship and Critical Ice Shape Acquisition in CIRA-IWT Icing Wind Tunnel -- 1 Correlation Research Program -- 2 Standard Model Test -- 2.1 Test Model -- 2.2 Icing Parameters Sensitivity -- 2.3 Ice Shape Correlationship -- 3 Critical Ice Shape Research. 3.1 Critical Icing Conditions -- 3.2 Critical Ice Shape Test -- 4 Conclusion -- References -- Parametric Studies of the Fuselage Geometry of a Double-Bubble Aircraft Configuration -- 1 Introduction -- 2 Design Process -- 3 Numerical Analysis -- 3.1 Baseline Aircraft Geometry -- 3.2 Grid Generation -- 3.3 CFD Analysis -- 4 Results -- 4.1 Parametric Study on Fuselage Configuration -- 4.2 Design of Wing-Body Configuration -- 5 Conclusions -- References -- Wind Tunnel Free Flight Model Attitude Determination Based on Non-contact IR Optical Measurement -- 1 Introduction -- 2 OptiTrack System -- 2.1 System Composition -- 2.2 Specification -- 2.3 Camera Layout -- 3 Attitude Determination -- 4 Test Scheme -- 5 Test Results -- 5.1 Ground Tests -- 5.2 Dynamic Tests -- 6 Future Work -- 7 Conclusions -- References -- Design and Performance Analysis of a Fuel Cell Powered Heavy-Lift Multirotor Drone -- 1 Introduction -- 1.1 kW Fuel Cell System -- 2 Multicopter Design -- 2.1 Sizing and Weight Estimation -- 2.2 Propulsion System -- 2.3 System Controller -- 2.4 Structure Optimization -- 2.5 Airflow Design -- 3 Flight Test and Analysis -- 3.1 Flight Test Conditions -- 3.2 Flight Test Results -- 4 Flight Time Estimation -- 5 Conclusion -- References -- Multi-objective System Optimization of Suborbital Spaceplane by Multi-fidelity Aerodynamic Analysis -- 1 Introduction -- 2 Aerodynamic Calculation Methods -- 2.1 Low-Accuracy Aerodynamic Calculation Method -- 2.2 High-Accuracy Aerodynamic Calculation Method -- 3 Surrogate Model -- 3.1 Multi-fidelity -- 3.2 Surrogate Model for Aerodynamic Analysis -- 4 MDO of Suborbital Spaceplane with the Surrogate Model -- 4.1 Design Optimization Methodology -- 4.2 Design Analysis Models -- 5 Result and Discussions -- 5.1 Outline -- 5.2 Airframe and Trajectory -- 6 Conclusion -- References. Experimental Validation of Nonlinear Coupled Constitutive Relations in Continuum Flows. |
Record Nr. | UNINA-9910627237203321 |
Gateway East, Singapore : , : Springer, , [2023] | ||
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Lo trovi qui: Univ. Federico II | ||
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