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Aerospace structures and materials / / edited by Yucheng Liu
| Aerospace structures and materials / / edited by Yucheng Liu |
| Pubbl/distr/stampa | Sharjah, United Arab Emirates : , : Bentham eBooks, , 2016 |
| Descrizione fisica | 1 online resource (591 pages) : illustrations |
| Disciplina | 629.1341 |
| Collana | Frontiers in Aerospace Science |
| Soggetto topico |
Airplanes - Design and construction
Space vehicles - Materials |
| ISBN | 1-68108-305-1 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910798890603321 |
| Sharjah, United Arab Emirates : , : Bentham eBooks, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerospace structures and materials / / edited by Yucheng Liu
| Aerospace structures and materials / / edited by Yucheng Liu |
| Pubbl/distr/stampa | Sharjah, United Arab Emirates : , : Bentham eBooks, , 2016 |
| Descrizione fisica | 1 online resource (591 pages) : illustrations |
| Disciplina | 629.1341 |
| Collana | Frontiers in Aerospace Science |
| Soggetto topico |
Airplanes - Design and construction
Space vehicles - Materials |
| ISBN | 1-68108-305-1 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910809038403321 |
| Sharjah, United Arab Emirates : , : Bentham eBooks, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
An assessment of the state-of-the-art in the design and manufacturing of large composite structures for aerospace vehicles / / Charles E. Harris, James H. Starnes, and Mark J. Shuart
| An assessment of the state-of-the-art in the design and manufacturing of large composite structures for aerospace vehicles / / Charles E. Harris, James H. Starnes, and Mark J. Shuart |
| Autore | Harris Charles E. <1950-> |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2001 |
| Descrizione fisica | 1 online resource (45 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Design analysis
Manufacturing Structural design Polymer matrix composites Composite structures Aerospace planes Airplanes - Design and construction Composite materials Space vehicles - Materials |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910691729103321 |
Harris Charles E. <1950->
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2001 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Basic research and technologies for two-state-to-orbit vehicles [[electronic resource] ] : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner
| Basic research and technologies for two-state-to-orbit vehicles [[electronic resource] ] : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner |
| Pubbl/distr/stampa | Weinheim, : Wiley-VCH, c2005 |
| Descrizione fisica | 1 online resource (686 p.) |
| Disciplina |
629.4
629.47 |
| Altri autori (Persone) |
JacobDieter <1941->
SachsG (Gottfried) WagnerS <1937-2018.> (Siegfried) |
| Collana | Deutsche Forschung |
| Soggetto topico |
Space vehicles - Aerodynamics
Space vehicles - Design and construction Space vehicles - Materials Space vehicles - Thermodynamics |
| ISBN |
1-280-52056-6
9786610520565 3-527-60571-1 3-527-60550-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Basic Research and Technologies for Two-Stage-to-Orbit Vehicles; Contents; 1 Introduction; 2 Network Organization of Collaborative Research Centres for Scientific Efficiency Enhancement; 2.1 Introduction; 2.2 Organization of Collaboration; 2.3 Efficiency Enhancement in Research; 2.4 Efficiency Enhancement in Teaching and Education; 2.5 Internationalization; 2.6 Final Remarks; 3 Overall Design Aspects; 3.1 Conceptual Design of Winged Reusable Two-Stage-to-Orbit Space Transport Systems; 3.1.1 Background and Introduction; 3.1.2 Concepts for Reusable Space Transports
3.1.2.1 Single-Stage-to-Orbit SSTO3.1.2.2 Two-Stage-to-Orbit TSTO; 3.1.3 Design Procedure; 3.1.3.1 Design Tools and Methods; 3.1.3.2 Baseline Concept; 3.1.3.3 Boundary Conditions and Requirements; 3.1.3.4 Variation of Mission and Staging Mach Number; 3.1.3.5 Trade Studies; 3.1.3.6 Evaluation and Comparison of the Concepts; 3.1.4 Variation of Mission and Mach Numbers; 3.1.4.1 Mission Comparison; 3.1.4.2 Comparison of Mach Number Variation; 3.1.4.3 Accelerator Vehicle Concepts; 3.1.5 Trade Studies; 3.1.5.1 Airbreathing Second Stage; 3.1.5.2 LOX-Collection; 3.1.6 Comparison and Evaluation 3.1.7 Conclusion and Outlook3.2 Evaluation and Multidisciplinary Optimization of Two-Stage-to-Orbit Space Planes with Different Lower-Stage Concepts; 3.2.1 Introduction; 3.2.2 Reference Configurations; 3.2.2.1 Concept Design and Mission Requirements; 3.2.2.2 Space Plane Configuration with Lifting Body Lower Stage; 3.2.2.3 Space Plane Configuration with Waverider Lower Stage; 3.2.2.4 Design and Optimization Parameters; 3.2.3 Analysis Methods; 3.2.3.1 Quality Criteria; 3.2.3.2 Simulation and Optimization Software; 3.2.4 Performance of Reference Space Planes; 3.2.4.1 Mass Breakdown 3.2.4.2 Design Sensitivities3.2.5 Optimization Results; 3.2.5.1 Nominal Optimizations; 3.2.5.2 Sensitivity-Based Optimizations; 3.2.6 Summary and Conclusions; 4 Aerodynamics and Thermodynamics; 4.1 Low-Speed Tests with an ELAC-Model at High Reynolds Numbers; 4.1.1 Introduction; 4.1.2 Wind Tunnel Models; 4.1.3 Pressure Distributions Influenced by Reynolds Number; 4.1.4 Flow Field Influenced by Reynolds Number; 4.1.5 Force Coefficients Influenced by Reynolds Number; 4.1.6 Conclusion; 4.2 Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration; 4.2.1 Introduction 4.2.2 Experimental Setup4.2.3 Numerical Method; 4.2.4 Results; 4.2.4.1 Flow Over the Orbital Stage and the EOS/Flat Plate Configuration; 4.2.4.2 Separation of ELAC1C and EOS; 4.2.5 Conclusions; 4.3 Stage Separation - Aerodynamics and Flow Physics; 4.3.1 Introduction; 4.3.2 Methodology and Vehicle Geometries; 4.3.3 Numerical Simulation; 4.3.3.1 Flow Solver; 4.3.3.2 Grid Generation; 4.3.4 Experimental Simulation; 4.3.4.1 Models and Facility; 4.3.4.2 Measurement Technique and Test Programme; 4.3.5 Steady State Flow; 4.3.5.1 Dominant Flow Phenomena; 4.3.5.1.1 Inviscid Case - 2D and 3D Simulations 4.3.5.1.2 Viscous Effects - Laminar and Turbulent Flow |
| Record Nr. | UNINA-9910144586203321 |
| Weinheim, : Wiley-VCH, c2005 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Basic research and technologies for two-state-to-orbit vehicles [[electronic resource] ] : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner
| Basic research and technologies for two-state-to-orbit vehicles [[electronic resource] ] : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner |
| Pubbl/distr/stampa | Weinheim, : Wiley-VCH, c2005 |
| Descrizione fisica | 1 online resource (686 p.) |
| Disciplina |
629.4
629.47 |
| Altri autori (Persone) |
JacobDieter <1941->
SachsG (Gottfried) WagnerS <1937-2018.> (Siegfried) |
| Collana | Deutsche Forschung |
| Soggetto topico |
Space vehicles - Aerodynamics
Space vehicles - Design and construction Space vehicles - Materials Space vehicles - Thermodynamics |
| ISBN |
1-280-52056-6
9786610520565 3-527-60571-1 3-527-60550-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Basic Research and Technologies for Two-Stage-to-Orbit Vehicles; Contents; 1 Introduction; 2 Network Organization of Collaborative Research Centres for Scientific Efficiency Enhancement; 2.1 Introduction; 2.2 Organization of Collaboration; 2.3 Efficiency Enhancement in Research; 2.4 Efficiency Enhancement in Teaching and Education; 2.5 Internationalization; 2.6 Final Remarks; 3 Overall Design Aspects; 3.1 Conceptual Design of Winged Reusable Two-Stage-to-Orbit Space Transport Systems; 3.1.1 Background and Introduction; 3.1.2 Concepts for Reusable Space Transports
3.1.2.1 Single-Stage-to-Orbit SSTO3.1.2.2 Two-Stage-to-Orbit TSTO; 3.1.3 Design Procedure; 3.1.3.1 Design Tools and Methods; 3.1.3.2 Baseline Concept; 3.1.3.3 Boundary Conditions and Requirements; 3.1.3.4 Variation of Mission and Staging Mach Number; 3.1.3.5 Trade Studies; 3.1.3.6 Evaluation and Comparison of the Concepts; 3.1.4 Variation of Mission and Mach Numbers; 3.1.4.1 Mission Comparison; 3.1.4.2 Comparison of Mach Number Variation; 3.1.4.3 Accelerator Vehicle Concepts; 3.1.5 Trade Studies; 3.1.5.1 Airbreathing Second Stage; 3.1.5.2 LOX-Collection; 3.1.6 Comparison and Evaluation 3.1.7 Conclusion and Outlook3.2 Evaluation and Multidisciplinary Optimization of Two-Stage-to-Orbit Space Planes with Different Lower-Stage Concepts; 3.2.1 Introduction; 3.2.2 Reference Configurations; 3.2.2.1 Concept Design and Mission Requirements; 3.2.2.2 Space Plane Configuration with Lifting Body Lower Stage; 3.2.2.3 Space Plane Configuration with Waverider Lower Stage; 3.2.2.4 Design and Optimization Parameters; 3.2.3 Analysis Methods; 3.2.3.1 Quality Criteria; 3.2.3.2 Simulation and Optimization Software; 3.2.4 Performance of Reference Space Planes; 3.2.4.1 Mass Breakdown 3.2.4.2 Design Sensitivities3.2.5 Optimization Results; 3.2.5.1 Nominal Optimizations; 3.2.5.2 Sensitivity-Based Optimizations; 3.2.6 Summary and Conclusions; 4 Aerodynamics and Thermodynamics; 4.1 Low-Speed Tests with an ELAC-Model at High Reynolds Numbers; 4.1.1 Introduction; 4.1.2 Wind Tunnel Models; 4.1.3 Pressure Distributions Influenced by Reynolds Number; 4.1.4 Flow Field Influenced by Reynolds Number; 4.1.5 Force Coefficients Influenced by Reynolds Number; 4.1.6 Conclusion; 4.2 Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration; 4.2.1 Introduction 4.2.2 Experimental Setup4.2.3 Numerical Method; 4.2.4 Results; 4.2.4.1 Flow Over the Orbital Stage and the EOS/Flat Plate Configuration; 4.2.4.2 Separation of ELAC1C and EOS; 4.2.5 Conclusions; 4.3 Stage Separation - Aerodynamics and Flow Physics; 4.3.1 Introduction; 4.3.2 Methodology and Vehicle Geometries; 4.3.3 Numerical Simulation; 4.3.3.1 Flow Solver; 4.3.3.2 Grid Generation; 4.3.4 Experimental Simulation; 4.3.4.1 Models and Facility; 4.3.4.2 Measurement Technique and Test Programme; 4.3.5 Steady State Flow; 4.3.5.1 Dominant Flow Phenomena; 4.3.5.1.1 Inviscid Case - 2D and 3D Simulations 4.3.5.1.2 Viscous Effects - Laminar and Turbulent Flow |
| Record Nr. | UNINA-9910830287803321 |
| Weinheim, : Wiley-VCH, c2005 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Basic research and technologies for two-state-to-orbit vehicles : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner
| Basic research and technologies for two-state-to-orbit vehicles : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner |
| Pubbl/distr/stampa | Weinheim, : Wiley-VCH, c2005 |
| Descrizione fisica | 1 online resource (686 p.) |
| Disciplina |
629.4
629.47 |
| Altri autori (Persone) |
JacobDieter
SachsG (Gottfried) WagnerSiegfried |
| Collana | Deutsche Forschung |
| Soggetto topico |
Space vehicles - Aerodynamics
Space vehicles - Design and construction Space vehicles - Materials Space vehicles - Thermodynamics |
| ISBN |
1-280-52056-6
9786610520565 3-527-60571-1 3-527-60550-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Basic Research and Technologies for Two-Stage-to-Orbit Vehicles; Contents; 1 Introduction; 2 Network Organization of Collaborative Research Centres for Scientific Efficiency Enhancement; 2.1 Introduction; 2.2 Organization of Collaboration; 2.3 Efficiency Enhancement in Research; 2.4 Efficiency Enhancement in Teaching and Education; 2.5 Internationalization; 2.6 Final Remarks; 3 Overall Design Aspects; 3.1 Conceptual Design of Winged Reusable Two-Stage-to-Orbit Space Transport Systems; 3.1.1 Background and Introduction; 3.1.2 Concepts for Reusable Space Transports
3.1.2.1 Single-Stage-to-Orbit SSTO3.1.2.2 Two-Stage-to-Orbit TSTO; 3.1.3 Design Procedure; 3.1.3.1 Design Tools and Methods; 3.1.3.2 Baseline Concept; 3.1.3.3 Boundary Conditions and Requirements; 3.1.3.4 Variation of Mission and Staging Mach Number; 3.1.3.5 Trade Studies; 3.1.3.6 Evaluation and Comparison of the Concepts; 3.1.4 Variation of Mission and Mach Numbers; 3.1.4.1 Mission Comparison; 3.1.4.2 Comparison of Mach Number Variation; 3.1.4.3 Accelerator Vehicle Concepts; 3.1.5 Trade Studies; 3.1.5.1 Airbreathing Second Stage; 3.1.5.2 LOX-Collection; 3.1.6 Comparison and Evaluation 3.1.7 Conclusion and Outlook3.2 Evaluation and Multidisciplinary Optimization of Two-Stage-to-Orbit Space Planes with Different Lower-Stage Concepts; 3.2.1 Introduction; 3.2.2 Reference Configurations; 3.2.2.1 Concept Design and Mission Requirements; 3.2.2.2 Space Plane Configuration with Lifting Body Lower Stage; 3.2.2.3 Space Plane Configuration with Waverider Lower Stage; 3.2.2.4 Design and Optimization Parameters; 3.2.3 Analysis Methods; 3.2.3.1 Quality Criteria; 3.2.3.2 Simulation and Optimization Software; 3.2.4 Performance of Reference Space Planes; 3.2.4.1 Mass Breakdown 3.2.4.2 Design Sensitivities3.2.5 Optimization Results; 3.2.5.1 Nominal Optimizations; 3.2.5.2 Sensitivity-Based Optimizations; 3.2.6 Summary and Conclusions; 4 Aerodynamics and Thermodynamics; 4.1 Low-Speed Tests with an ELAC-Model at High Reynolds Numbers; 4.1.1 Introduction; 4.1.2 Wind Tunnel Models; 4.1.3 Pressure Distributions Influenced by Reynolds Number; 4.1.4 Flow Field Influenced by Reynolds Number; 4.1.5 Force Coefficients Influenced by Reynolds Number; 4.1.6 Conclusion; 4.2 Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration; 4.2.1 Introduction 4.2.2 Experimental Setup4.2.3 Numerical Method; 4.2.4 Results; 4.2.4.1 Flow Over the Orbital Stage and the EOS/Flat Plate Configuration; 4.2.4.2 Separation of ELAC1C and EOS; 4.2.5 Conclusions; 4.3 Stage Separation - Aerodynamics and Flow Physics; 4.3.1 Introduction; 4.3.2 Methodology and Vehicle Geometries; 4.3.3 Numerical Simulation; 4.3.3.1 Flow Solver; 4.3.3.2 Grid Generation; 4.3.4 Experimental Simulation; 4.3.4.1 Models and Facility; 4.3.4.2 Measurement Technique and Test Programme; 4.3.5 Steady State Flow; 4.3.5.1 Dominant Flow Phenomena; 4.3.5.1.1 Inviscid Case - 2D and 3D Simulations 4.3.5.1.2 Viscous Effects - Laminar and Turbulent Flow |
| Record Nr. | UNINA-9910876530003321 |
| Weinheim, : Wiley-VCH, c2005 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Effect of plug and shroud geometry variables on plug-nozzle performance at transonic speeds / / by Bobby L. Berrier
| Effect of plug and shroud geometry variables on plug-nozzle performance at transonic speeds / / by Bobby L. Berrier |
| Autore | Berrier Bobby L. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , March 1969 |
| Descrizione fisica | 1 online resource (195 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Transonic speed
Plugs Powder metallurgy Space vehicles - Materials |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716055303321 |
|
Berrier Bobby L.
|
||
| Washington, D.C. : , : National Aeronautics and Space Administration, , March 1969 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Gossamer spacecraft [[electronic resource] ] : membrane and inflatable structures technology for space applications / / edited by Christopher H.M. Jenkins
| Gossamer spacecraft [[electronic resource] ] : membrane and inflatable structures technology for space applications / / edited by Christopher H.M. Jenkins |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2001 |
| Descrizione fisica | 1 online resource (604 p.) |
| Disciplina |
629.1 s
629.47 |
| Altri autori (Persone) | JenkinsC. H |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Expandable space structures
Space vehicles - Materials Membranes (Technology) |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-661-1
1-60086-442-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter 1. Overview of Gossamer Structures""; ""I. Background""; ""II. Applications""; ""A. Solar Arrays""; ""B. Communication Systems""; ""C. Human Habitats""; ""D. Planetary Surface Exploration""; ""E. Radar and Reflect Arrays""; ""F. Solar Concentrators""; ""G. Solar Shades""; ""III. Membranes for Gossamer Structures""; ""IV. Rigidization Technology""; ""V. Analysis and Modeling of Gossamer Structures""; ""VI. Adaptive, Smart, and Multifunctional Gossamer Systems""
""A. Adaptive Compensation of Membrane Reflectors""""B. Multifunctional Membranes""; ""C. Smart Structures""; ""VII. Summary""; ""Acknowledgments""; ""Chapter 2. History of Relevant Inflatable High-Precision Space Structures Technology Developments""; ""I. Introduction""; ""II. Goodyear's Inflatable Structures""; ""A. Inflatable Search Radar Antenna""; ""B. Radar Calibration Sphere""; ""C. Lenticular Inflatable Parabolic Reflector""; ""D. Echo Balloons""; ""E. Contraves Inflatable Structures"" ""F. Reflector Antenna Concepts for Very Large Baseline Interferometry and Land Mobile Communications""""G. Telescope Sunshade Support Structure""; ""III. L' Garde Inc.'s Inflatable Space Structures""; ""A. L' Garde Inc.'s Simulated Decoys""; ""B. Large Offset Reflector Structure""; ""C. Inflatable Antenna Experiment""; ""IV. ILC Dover's Inflatable Space Structures""; ""A. Large Solar-Array Structure""; ""V. Other Organizations with Inflatable Space Structures Technology Capability""; ""References""; ""Chapter 3. Mechanics of Membrane Structures""; ""Nomenclature""; ""I. Introduction"" ""A. Definition and Unique Behavior of Membranes""""B. Tensor Analysis""; ""C. Coordinate Systems and Configurations""; ""II. Kinematics of Deformation""; ""A. Motion and Deformation""; ""B. Deformation Gradient, Stretch, and Polar Decomposition""; ""C. Strain Definitions""; ""D. Deformation and Strain Rate""; ""III. Stress and Balance Laws""; ""A. Concept of Stress""; ""B. Stress Definitions""; ""C. Mass Balance""; ""D. Momentum Balance""; ""E. Energy Balance""; ""F. Conjugate Stress and Strain""; ""IV. Constitutive Equations""; ""A. Introduction""; ""B. Thermomechanics"" ""C. Thermomechanic Field Theory""""D. Constitutive Relations for Elastic Solids and Sheets""; ""E. Constitutive Laws for Viscoelastic Materials""; ""F. Bodner�Partom�Rubin Model""; ""G. Fabrics""; ""V. Approximations""; ""A. Approximations in the Era of Computational Mechanics""; ""B. Nonlinear Nature of Membrane Problems""; ""C. Approximations in the Context of the Governing Equations""; ""D. Example""; ""E. On Accuracy and Modeling""; ""VI. Analysis of Wrinkled Membranes""; ""A. Introduction""; ""B. Tension-Field Modeling via a Penalty Parameter Modified Constitutive Law"" ""VII. Experimental Analysis"" |
| Record Nr. | UNINA-9910457704403321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2001 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Gossamer spacecraft [[electronic resource] ] : membrane and inflatable structures technology for space applications / / edited by Christopher H.M. Jenkins
| Gossamer spacecraft [[electronic resource] ] : membrane and inflatable structures technology for space applications / / edited by Christopher H.M. Jenkins |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2001 |
| Descrizione fisica | 1 online resource (604 p.) |
| Disciplina |
629.1 s
629.47 |
| Altri autori (Persone) | JenkinsC. H |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Expandable space structures
Space vehicles - Materials Membranes (Technology) |
| ISBN |
1-60086-661-1
1-60086-442-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter 1. Overview of Gossamer Structures""; ""I. Background""; ""II. Applications""; ""A. Solar Arrays""; ""B. Communication Systems""; ""C. Human Habitats""; ""D. Planetary Surface Exploration""; ""E. Radar and Reflect Arrays""; ""F. Solar Concentrators""; ""G. Solar Shades""; ""III. Membranes for Gossamer Structures""; ""IV. Rigidization Technology""; ""V. Analysis and Modeling of Gossamer Structures""; ""VI. Adaptive, Smart, and Multifunctional Gossamer Systems""
""A. Adaptive Compensation of Membrane Reflectors""""B. Multifunctional Membranes""; ""C. Smart Structures""; ""VII. Summary""; ""Acknowledgments""; ""Chapter 2. History of Relevant Inflatable High-Precision Space Structures Technology Developments""; ""I. Introduction""; ""II. Goodyear's Inflatable Structures""; ""A. Inflatable Search Radar Antenna""; ""B. Radar Calibration Sphere""; ""C. Lenticular Inflatable Parabolic Reflector""; ""D. Echo Balloons""; ""E. Contraves Inflatable Structures"" ""F. Reflector Antenna Concepts for Very Large Baseline Interferometry and Land Mobile Communications""""G. Telescope Sunshade Support Structure""; ""III. L' Garde Inc.'s Inflatable Space Structures""; ""A. L' Garde Inc.'s Simulated Decoys""; ""B. Large Offset Reflector Structure""; ""C. Inflatable Antenna Experiment""; ""IV. ILC Dover's Inflatable Space Structures""; ""A. Large Solar-Array Structure""; ""V. Other Organizations with Inflatable Space Structures Technology Capability""; ""References""; ""Chapter 3. Mechanics of Membrane Structures""; ""Nomenclature""; ""I. Introduction"" ""A. Definition and Unique Behavior of Membranes""""B. Tensor Analysis""; ""C. Coordinate Systems and Configurations""; ""II. Kinematics of Deformation""; ""A. Motion and Deformation""; ""B. Deformation Gradient, Stretch, and Polar Decomposition""; ""C. Strain Definitions""; ""D. Deformation and Strain Rate""; ""III. Stress and Balance Laws""; ""A. Concept of Stress""; ""B. Stress Definitions""; ""C. Mass Balance""; ""D. Momentum Balance""; ""E. Energy Balance""; ""F. Conjugate Stress and Strain""; ""IV. Constitutive Equations""; ""A. Introduction""; ""B. Thermomechanics"" ""C. Thermomechanic Field Theory""""D. Constitutive Relations for Elastic Solids and Sheets""; ""E. Constitutive Laws for Viscoelastic Materials""; ""F. Bodner�Partom�Rubin Model""; ""G. Fabrics""; ""V. Approximations""; ""A. Approximations in the Era of Computational Mechanics""; ""B. Nonlinear Nature of Membrane Problems""; ""C. Approximations in the Context of the Governing Equations""; ""D. Example""; ""E. On Accuracy and Modeling""; ""VI. Analysis of Wrinkled Membranes""; ""A. Introduction""; ""B. Tension-Field Modeling via a Penalty Parameter Modified Constitutive Law"" ""VII. Experimental Analysis"" |
| Record Nr. | UNINA-9910781540103321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2001 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
High performance materials in aerospace / edited by Harvey M. Flower
| High performance materials in aerospace / edited by Harvey M. Flower |
| Pubbl/distr/stampa | Dordrecht : Springer-Science+Business Media, 1995 |
| Descrizione fisica | x, 382 p. ; 25 cm |
| Disciplina | 629.134 |
| Altri autori (Persone) | Flower, Harvey M. |
| Soggetto topico |
Airplanes - Materials
Space vehicles - Materials Physical metallurgy |
| ISBN | 9789401042963 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991002123699707536 |
| Dordrecht : Springer-Science+Business Media, 1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Salento | ||
| ||
