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Journal of aerospace engineering
| Journal of aerospace engineering |
| Pubbl/distr/stampa | New York, N.Y., : American Society of Civil Engineers, Aerospace Division |
| Disciplina | 629.1 |
| Soggetto topico |
Astronautics
Aerospace engineering Civil engineering |
| ISSN | 1943-5525 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Periodico |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910338731403321 |
| New York, N.Y., : American Society of Civil Engineers, Aerospace Division | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Journal of guidance and control
| Journal of guidance and control |
| Pubbl/distr/stampa | New York, : American Institute of Aeronautics and Astronautics |
| Disciplina | 629.1 |
| ISSN | 0162-3192 |
| Formato | Materiale a stampa |
| Livello bibliografico | Periodico |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-990008989270403321 |
| New York, : American Institute of Aeronautics and Astronautics | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Key Basic Scientific Problems on near-Space Vehicles / / Shanyi Du, editor
| Key Basic Scientific Problems on near-Space Vehicles / / Shanyi Du, editor |
| Edizione | [First edition.] |
| Pubbl/distr/stampa | Singapore : , : Springer, , [2023] |
| Descrizione fisica | 1 online resource (XIX, 119 p. 16 illus., 10 illus. in color.) |
| Disciplina | 629.1 |
| Collana | Reports of China's Basic Research Series |
| Soggetto topico |
Aerospace engineering
Aerospace engineering - China |
| ISBN | 981-19-8907-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Project Overview -- Research Status at Home and Abroad -- Major Research Achievements -- Outlook. |
| Record Nr. | UNINA-9910686776303321 |
| Singapore : , : Springer, , [2023] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The Last of NASA's Original Pilot Astronauts [[electronic resource] ] : Expanding the Space Frontier in the Late Sixties / / by David J. Shayler, Colin Burgess
| The Last of NASA's Original Pilot Astronauts [[electronic resource] ] : Expanding the Space Frontier in the Late Sixties / / by David J. Shayler, Colin Burgess |
| Autore | Shayler David J |
| Edizione | [1st ed. 2017.] |
| Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2017 |
| Descrizione fisica | 1 online resource (XXVIII, 427 p. 74 illus., 45 illus. in color.) |
| Disciplina | 629.1 |
| Collana | Space Exploration |
| Soggetto topico |
Aerospace engineering
Astronautics Space sciences Aerospace Technology and Astronautics Space Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics) |
| ISBN | 3-319-51014-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Chapter 1: The Selections -- Chapter 2: The Nineteen -- Chapter 3: The Almost Astronauts -- Chapter 4: Preparing for Apollo -- Chapter 5: Supporting Apollo -- Chapter 6: Before this Decade is Out -- Chapter 7: Preparing for MOL -- Chapter 8: NASA's MOL(mag)nificent Seven -- Chapter 9: Where Blue Skies Turn Black -- Chapter 10: Riding 'The Stack' -- Chapter 11: After Space -- Afterword -- Appendices -- Bibliography -- About the Authors -- Other Works by the Authors -- Index. |
| Record Nr. | UNINA-9910254575403321 |
Shayler David J
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| Cham : , : Springer International Publishing : , : Imprint : Springer, , 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Le ballon, l'avion, la route aérienne / par Maurice Larrouy
| Le ballon, l'avion, la route aérienne / par Maurice Larrouy |
| Autore | Larrouy, Maurice |
| Pubbl/distr/stampa | Paris : A. Colin, 1923 |
| Descrizione fisica | VIII, 215 p. ; 18 cm |
| Disciplina | 629.1 |
| Collana | Collection Armand Colin, Section des arts militaires |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | fre |
| Record Nr. | UNIPARTHENOPE-000010023 |
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Larrouy, Maurice
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| Paris : A. Colin, 1923 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Parthenope | ||
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Lecture Notes in Rotorcraft Engineering [[electronic resource] /] / edited by Antonio Filippone, George Barakos
| Lecture Notes in Rotorcraft Engineering [[electronic resource] /] / edited by Antonio Filippone, George Barakos |
| Edizione | [1st ed. 2023.] |
| Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2023 |
| Descrizione fisica | 1 online resource (255 pages) |
| Disciplina | 629.1 |
| Collana | Springer Aerospace Technology |
| Soggetto topico |
Aerospace engineering
Astronautics Aerospace Technology and Astronautics |
| ISBN | 3-031-12437-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Rotor Aerodynamics -- Experimental methods for rotor aerodynamics -- Rotorcraft Propulsion Systems -- Rotorcraft Flight Performance -- Tilt-rotor aeromechanics -- Rotor acoustics -- Rotorcraft control systems -- Rotorcraft Preliminary Design -- Appendix A: Numerical Solution of Acoustic Problems -- Index. |
| Record Nr. | UNINA-9910647398803321 |
| Cham : , : Springer International Publishing : , : Imprint : Springer, , 2023 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Life Cycle Assessment in Aviation [[electronic resource] ] : Theory and Applications / / edited by T. Hikmet Karakoc, Selçuk Ekici, Alper Dalkiran
| Life Cycle Assessment in Aviation [[electronic resource] ] : Theory and Applications / / edited by T. Hikmet Karakoc, Selçuk Ekici, Alper Dalkiran |
| Autore | Karakoc T. Hikmet |
| Edizione | [1st ed. 2024.] |
| Pubbl/distr/stampa | Cham : , : Springer Nature Switzerland : , : Imprint : Springer, , 2024 |
| Descrizione fisica | 1 online resource (121 pages) |
| Disciplina | 629.1 |
| Altri autori (Persone) |
EkiciSelçuk
DalkiranAlper |
| Collana | Sustainable Aviation |
| Soggetto topico |
Aerospace engineering
Astronautics Sustainability Environmental management Renewable energy sources Energy policy Energy and state Aerospace Technology and Astronautics Environmental Management Renewable Energy Energy Policy, Economics and Management |
| ISBN | 3-031-52772-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Chapter 1. Life Cycle Analysis (LCA): A retrospective overview -- Chapter 2. Life Cycle Assessment – A Brief Definition and Overview -- Chapter 3. Application of LCA to Aviation -- Chapter 4. Application of LCA to Aviation Fuels -- Chapter 5. Life Cycle Assessment (LCA) Applications in Airports -- Chapter 6. Exergoenvironmental analysis of Medium-Size Turboprop Engine (m-TPE) based Life Cycle Analysis (LCA) and Exergy. |
| Record Nr. | UNINA-9910845097803321 |
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Karakoc T. Hikmet
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| Cham : , : Springer Nature Switzerland : , : Imprint : Springer, , 2024 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Lighter than air systems : proceedings of the international conference on design and engineering of lighter-than-air systems 2022 (DELTAs-2022) / / Dhwanil Shukla, editor
| Lighter than air systems : proceedings of the international conference on design and engineering of lighter-than-air systems 2022 (DELTAs-2022) / / Dhwanil Shukla, editor |
| Pubbl/distr/stampa | Singapore : , : Springer, , [2023] |
| Descrizione fisica | 1 online resource (267 pages) |
| Disciplina | 629.1 |
| Collana | Lecture notes in mechanical engineering |
| Soggetto topico |
Aeronautics
Airships |
| ISBN |
9789811960499
9789811960482 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Intro -- Conference Committee -- Reviewers -- Preface -- Contents -- About the Editor -- Effect of Geometrical Parameters of a Tethered Aerostat on Longitudinal Stability Boundaries -- 1 Introduction -- 2 Mathematical Modeling -- 2.1 Aerodynamic Forces and Moments -- 2.2 Tether Cable Forces and Moments -- 2.3 Buoyancy Forces and Moments -- 2.4 Gravity Forces and Moments -- 3 Estimation of the Stability Characteristics -- 3.1 Balloon Equations of Motion -- 3.2 Equilibrium Trim Conditions -- 3.3 Formulations for Calculation of Stability Derivatives -- 3.4 Equilibrium Cable Shape -- 3.5 Cable Force Derivatives -- 3.6 Stability Equations (Longitudinal) -- 4 Effect of Geometrical Parameters on Longitudinal Stability Boundaries -- 5 Conclusion -- References -- CPACS LTA-Using Common Data Structures for Visualization and Optimization of Airship Designs -- 1 Introduction -- 1.1 Background -- 1.2 Objectives -- 2 Problem Definition and Formulation -- 3 Methodology -- 3.1 Airship Modeling -- 3.2 Parameter Estimation -- 3.3 Design Optimization -- 4 Results -- 5 Discussion and Conclusions -- References -- Airship Sling-Load Operations: A Model Flight-Test Approach -- 1 Introduction -- 1.1 Background -- 1.2 Objectives -- 2 Problem Definition and Formulation -- 2.1 Load Exchange and Certification -- 2.2 Maneuverability -- 3 Methodology -- 3.1 Sling-Load Operation -- 3.2 Model Flight-Test -- 4 Results -- 4.1 Cruise Mode -- 4.2 Dynamic Positioning -- 5 Discussion and Conclusions -- 5.1 Discussion -- 5.2 Conclusion -- References -- Optimization of TPU/TiO2 Films Using UV Additives for Improved Weather Stability of LTA Hull Materials -- 1 Introduction -- 2 Methodology -- 2.1 Materials -- 2.2 Method of Preparation of Films -- 2.3 UV-VIS Spectroscopy -- 2.4 Fourier Transform Infra-Red Spectroscopy (FTIR) -- 2.5 Artificial Accelerated Weathering -- 2.6 UPF Measurement.
2.7 Yellowness Index -- 2.8 Gas Barrier Measurement -- 2.9 Tensile Testing of Films -- 3 Results and Discussion -- 3.1 UV-VIS Spectroscopy -- 3.2 Fourier Transform Infra-Red Spectroscopy -- 3.3 UPF Measurement -- 3.4 Yellowness Index -- 3.5 Gas Barrier Properties -- 3.6 Tensile Testing -- 4 Future Scope -- 5 Conclusion -- References -- Airship Turn Performance Estimated From Efficient Potential Flow Panel Method -- 1 Introduction -- 2 Problem Definition and Formulation -- 3 Methodology -- 4 Results -- 5 Discussion and Conclusions -- References -- Evaluation of High-Performance Fabric-Based Laminated Hull Material for High-Altitude Airship -- 1 Introduction -- 1.1 High-Altitude Airship System -- 2 Materials and Methods -- 2.1 Materials -- 2.2 Methods -- 3 Characterizations and Testing -- 3.1 Wide Angle X-ray Diffraction (XRD) -- 3.2 Differential Scanning Calorimetry (DSC) -- 3.3 Drop Shape Analyzer (DSA) -- 3.4 Atomic Force Microscopy (AFM) -- 3.5 T-Peel Test -- 3.6 Tensile Test -- 3.7 Tearing Test -- 3.8 Helium Gas Permeability Test -- 3.9 UV Protection Factor (UPF) -- 4 Results and Discussion -- 4.1 XRD Study -- 4.2 DSC Study -- 4.3 Helium Gas Permeability -- 4.4 Adhesion Studies -- 4.5 AFM Analysis -- 4.6 Effect of Crosslinker on Peel Strength -- 5 Study on Adhesive-Coated and Laminated Fabrics -- 5.1 Thickness and Weight of the Laminates -- 5.2 Effect of UV Additive on Peel Strength -- 5.3 Effect of UV Additive and Accelerated Weathering on UPF Value -- 5.4 Effect of Plasma Treatment on Peel Strength -- 5.5 Effect of Accelerated Weathering on Peel Strength -- 5.6 Effect of Water Soaking on Peel Strength -- 5.7 Effect of Accelerated Weathering on Tensile Properties -- 5.8 Effect of Accelerated Weathering on Tearing Strength -- 5.9 Effect of Accelerated Weathering on Gas Barrier Property -- 6 Butt Joint Strength -- 7 Conclusion -- References. Look Ahead Steering-Based Path Following Control for an Airship -- 1 Introduction -- 2 Airship Model -- 2.1 Linearization of Equations of Motion -- 3 Automatic Flight Control System -- 3.1 Guidance and Navigation Algorithm -- 3.2 Reference Model -- 3.3 Control System Design -- 4 Simulation Results -- 5 Conclusion -- References -- Functionalization of Polyurethane-Based Adhesives with UV Additives for LTA Applications -- 1 Introduction -- 2 Problem Definition and Formulation -- 3 Experimental -- 3.1 Materials -- 3.2 Methods -- 4 Characterization and Testing -- 4.1 ATR-FTIR -- 4.2 Tensile Testing and Peel Strength Testing -- 4.3 Helium Gas Permeability -- 4.4 Ultraviolet Protection Factor (UPF) -- 4.5 Differential Scanning Calorimetry (DSC) -- 4.6 Thermogravimetric Analysis (TGA) -- 5 Results and Discussion -- 5.1 Fourier Transform Infrared Spectroscopy (FTIR) Analysis -- 5.2 Peel Strength Test -- 5.3 Helium Permeability Testing -- 5.4 UV Protection Factor (UPF) Analysis -- 5.5 Thermogravimetric Analysis (TGA) -- 5.6 Differential Scanning Calorimetry (DSC) Analysis -- 6 Conclusion -- References -- Degradation Study of Aromatic and Aliphatic TPU Films in Accelerated Weathering: Impact on the Gas Barrier and Mechanical Properties -- 1 Introduction -- 2 Material and Method -- 2.1 Materials -- 2.2 TPU Extrusion Cast Film Preparation -- 2.3 Artificial Accelerated Weathering Test -- 2.4 Characterization Techniques -- 3 Results and Discussion -- 3.1 Mechanical Properties -- 3.2 Helium Gas Permeability -- 3.3 Surface Degradation -- 3.4 Chemical Structure -- 3.5 UPF Measurement -- 4 Conclusion -- References -- A Multidisciplinary Design Optimisation (MDO) Algorithm for the Automatic Sizing of an Unmanned Lighter-Than-Air Platform -- 1 Introduction -- 1.1 Problem Definition and Formulation -- 2 Methodology -- 3 Results. 3.1 Variation of Payload and Associated Power -- 3.2 Energy Systems -- 4 Discussion and Conclusions -- References -- The Concepts of Telescopic and Self-Deployable Tensegrity-Based Helium-Filled Aerostats -- 1 Introduction -- 2 The Concept of Adaptive Telescopic Aerostats -- 3 Comparison of Strategies for Control of Aerostat Motion -- 4 The Concept of Tensegrity-Based Aerostat -- 5 Strength Analysis of Tensegrity-Based Aerostat -- 6 Discussion and Conclusions -- References -- Numerical Investigation of Laminar to Turbulent Boundary Layer Transition Over Airship Envelopes -- 1 Introduction -- 2 Validation for Flat Plate Cases -- 3 Establishing Efficacy of OpenFOAM® for Bodies of Revolution -- 3.1 Drag Calculation of GNVR Envelope -- 3.2 Assumed Transition Point Approach for Zhiyuan-1 Envelope -- 3.3 Evaluation of Transition Turbulence Model for Zhiyuan-1 Envelope -- 3.4 Transition Analysis on Zhiyuan-1 Envelope at Angle of Attack -- 4 Conclusions -- References -- Designing Helium-Filled Aerostats Applying Scaling Procedure, Mini-Models CANDY and Fly-Tests on SKYLAB -- 1 Introduction -- 2 Testing V-Mobility Via Mini-Models CANDY -- 3 Volume Measurement by Optical Technique -- 4 The Scaling Procedure -- 5 The Case Studies -- 5.1 Numerical Model -- 5.2 Numerical Simulation of Aero-SDT Mission -- 6 Discussion and Conclusions -- References -- Effect of Reynolds Number on the Aerodynamic Characteristics of Leading-Edge Protuberanced Airship Fin -- 1 Introduction -- 2 Computational Methodology -- 3 Results and Discussion -- 3.1 Effect of Re on the Lift Characteristics Curve of LEP Fin -- 3.2 Effect of Re on the Drag Characteristics Curve of LEP Fin -- 4 Conclusion -- References -- Autonomous Tilt Rotor Stabilized Plimp Hybrid Airship Unmanned Aerial Vehicle -- 1 Literature Review -- 2 Introduction -- 3 Design -- 3.1 Material Selection. 3.2 Stability of Airship -- 3.3 The Various Forces and the Various Moments Acting on the Plimp -- 3.4 Plimp Stability from Designer Point of View -- 3.5 Requirements of the Hybrid VTOL Plimp Airship Unmanned Aerial Vehicle -- 4 Calculations -- 4.1 Weight Estimation -- 4.2 Airfoil Data for the Wing -- 4.3 Propeller Data -- 4.4 Different Phases of Flight -- 5 Mathematical Modeling and Autopilot Control System -- 6 Results -- 7 Summary -- 8 Conclusion -- References -- Numerical Approach to Maneuver Design and Feasibility Evaluation for the Autonomy of Airship -- 1 Introduction -- 2 6-DoF Aircraft Equations of Motion -- 2.1 Buoyant and Gravitational Terms -- 2.2 Aerodynamic and Control Terms -- 2.3 Propulsive Terms -- 3 Direct Continuation Methodology for Constrained Dynamical Systems -- 4 Maneuver Design with Feasibility Evaluation -- 4.1 Straight and Level Flight Maneuver -- 4.2 Level Turn Maneuver -- 4.3 Ascend and Descend Maneuvers -- 5 Validation -- 5.1 Level Performance Analysis -- 5.2 Ascend Maneuver Evaluation -- 6 Conclusions -- References -- Estimation of Stability Derivatives Due to Translational Motion of Various LTA Vehicles Using CFD -- 1 Introduction -- 2 Stability Derivatives Extraction Methodology -- 3 Aerostat Shapes -- 4 Numerical Simulation -- 4.1 Governing Equations -- 4.2 Computational Domain and Grid -- 5 Results and Discussion -- 5.1 Grid and Time Step Independence Study -- 5.2 Validation of the Grid Motion -- 5.3 Validation of the Stability Derivative Extraction Methodology -- 5.4 Acceleration and Frequency Independence Study -- 5.5 Zhiyuan Aerostat -- 5.6 GNVR, HAA and NPL Aerostats -- 6 Conclusions and Future Scope -- References. |
| Record Nr. | UNINA-9910633938703321 |
| Singapore : , : Springer, , [2023] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Low Earth Orbit Satellite Design / / George Sebestyen [et al.]
| Low Earth Orbit Satellite Design / / George Sebestyen [et al.] |
| Autore | Sebestyen George S |
| Edizione | [1st edition 2018.] |
| Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2018 |
| Descrizione fisica | 1 online resource (XIX, 317 pages) : 220 illustrations, 155 illustrations in color |
| Disciplina | 629.1 |
| Collana | Space Technology Library |
| Soggetto topico |
Aerospace engineering
Astronautics Space sciences Software engineering Aerospace Technology and Astronautics Space Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics) Software Engineering/Programming and Operating Systems |
| ISBN | 3-319-68315-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Preface -- About the Authors -- Chapter 1: Introduction -- Chapter 2: The Space Environment -- Chapter 3: Satellite Missions -- Chapter 4: Orbits and Space-Related Geometry -- Chapter 5: Electric Power Subsystem Design -- Chapter 6: Spacecraft Communications -- Chapter 7: Spacecraft Digital Hardware -- Chapter 8: Attitude Determination and Control Subsystem (ADACS) -- Chapter 9: Spacecraft Software -- Chapter 10: Spacecraft Structure -- Chapter 11: Deployment Mechanisms -- Chapter 12: Propulsion -- Chapter 13: Thermal Design -- Chapter 14: Radiation Hardening, Reliability and Redundancy -- Chapter 15: Integration and Test -- Chapter 16: Launch Vehicles and the Spacecraft Interfaces -- Chapter 17: Ground Stations and Ground Support Equipment -- Chapter 18: Spacecraft Operations -- Chapter 19: Low Cost Design and Development -- Chapter 20: Systems Engineering and Program Management -- Chapter 21: A Spacecraft Design Example -- Chapter 22: Downloadable Spreadsheets -- Appendix 1 -- Appendix 2 -- Appendix 3 -- Appendix 4 -- Appendix 5 -- Appendix 6 -- Appendix 7 -- Appendix 8 -- References -- Glossary -- Index. |
| Record Nr. | UNINA-9910299934303321 |
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Sebestyen George S
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| Cham : , : Springer International Publishing : , : Imprint : Springer, , 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Low Energy Flight: Orbital Dynamics and Mission Trajectory Design [[electronic resource] /] / by Jianping Yuan, Yu Cheng, Jinglang Feng, Chong Sun
| Low Energy Flight: Orbital Dynamics and Mission Trajectory Design [[electronic resource] /] / by Jianping Yuan, Yu Cheng, Jinglang Feng, Chong Sun |
| Autore | Yuan Jianping |
| Edizione | [1st ed. 2019.] |
| Pubbl/distr/stampa | Singapore : , : Springer Singapore : , : Imprint : Springer, , 2019 |
| Descrizione fisica | 1 online resource (X, 209 p. 136 illus., 108 illus. in color.) |
| Disciplina | 629.1 |
| Soggetto topico |
Aerospace engineering
Astronautics Mathematical physics Aerospace Technology and Astronautics Mathematical Applications in the Physical Sciences |
| ISBN | 981-13-6130-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- Continuous Low Thrust Trajectory Design and optimization -- Study of the Transfer Between Libration Point Orbits and Lunar Orbits in Earth-Moon System -- Lorentz Force Formation Flying in Earth-Moon System -- Orbital Dynamics in the Irregular Gravitational Field - Resonance -- Orbital Dynamics in the Vicinity of Contact Binary Asteroid Systems -- Appendices. |
| Record Nr. | UNINA-9910350289903321 |
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Yuan Jianping
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| Singapore : , : Springer Singapore : , : Imprint : Springer, , 2019 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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