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Modern aerodynamic methods for direct and inverse applications / / Wilson C. Chin
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.  
Hoboken, NJ : , : Wiley, , [2019]
Materiale a stampa
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Modern aerodynamic methods for direct and inverse applications / / Wilson C. Chin
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.  
Hoboken, NJ : , : Wiley, , [2019]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Modern compressible flow : with historical perspective / John D. Anderson, Jr.
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  
Boston : McGraw-Hill, 2004
Materiale a stampa
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
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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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
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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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
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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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
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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Noise resistance enhancement in aircraft navigation and connected systems / / Dmitry Alexandrovich Zatuchny [and four others]
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  
Gateway East, Singapore : , : Springer, , [2021]
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Noise Sources in Turbulent Shear Flows: Fundamentals and Applications / / edited by Roberto Camussi
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
Materiale a stampa
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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
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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