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Aerodynamic stability characteristics of the Apollo command module / / by William C. Moseley, Jr., Ralph E. Graham, and Jack E. Hughes
| Aerodynamic stability characteristics of the Apollo command module / / by William C. Moseley, Jr., Ralph E. Graham, and Jack E. Hughes |
| Autore | Moseley William C. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , August 1968 |
| Descrizione fisica | 1 online resource (xii, 171 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Wind tunnel testing
Space vehicles - Design and construction Stability of space vehicles |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715182103321 |
Moseley William C.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , August 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerospace engineering [[electronic resource] /] / SAE
| Aerospace engineering [[electronic resource] /] / SAE |
| Pubbl/distr/stampa | [Warrendale, Pa.], : [Society of Automotive Engineers] |
| Disciplina | 629.1/05 |
| Soggetto topico |
Airplanes - Design and construction
Space vehicles - Design and construction |
| ISSN | 2165-1167 |
| Formato | Materiale a stampa |
| Livello bibliografico | Periodico |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910438218503321 |
| [Warrendale, Pa.], : [Society of Automotive Engineers] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 | ||
| ||
Breaking the mishap chain : human factors lessons learned from aerospace accidents and incidents in research, flight test, and development / / Peter W. Merlin, Gregg A. Bendrick, Dwight A. Holland
| Breaking the mishap chain : human factors lessons learned from aerospace accidents and incidents in research, flight test, and development / / Peter W. Merlin, Gregg A. Bendrick, Dwight A. Holland |
| Autore | Merlin Peter W. <1964-> |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , 2012 |
| Descrizione fisica | 1 online resource (xv, 227 pages) : illustrations |
| Disciplina | 363.12/414 |
| Altri autori (Persone) |
BendrickGregg A
HollandDwight A |
| Collana | NASA aeronautics book series |
| Soggetto topico |
Aircraft accidents - Human factors
Research aircraft - Accidents Space vehicle accidents Research aircraft - Design and construction Space vehicles - Design and construction Aeronautics - Research Flight testing |
| Soggetto genere / forma | Case studies. |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Part 1. Design Factors -- "It May Not Be Hooked Up" : Automation Bias, Poor Communication, and Crew Resource Management Factors in the X-31Mishap -- Habit Pattern Transfer During the M2-F2 First Flight -- Pilot-Induced Oscillation During Space Shuttle Approach and Landing Tests -- Part 2. Physiological Factors -- Screening Versus Design : The X-15 Reentry Mishap -- Six Million Dollar Man : M2-F2 Task Saturation Mishap -- Almost-Loss of Consciousness in the F-22A Raptor -- Part 3. Organizational Factors -- Decision Chain Leading to the XB-70/F-104 Midair Collision -- Mission Management and Cockpit Resource Management in the B-1A Mishap -- Collision in Space : Human Factors in the Mir-Progress Mishap -- Conclusions. |
| Altri titoli varianti | Breaking the mishap chain |
| Record Nr. | UNINA-9910698791903321 |
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Merlin Peter W. <1964->
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| Washington, D.C. : , : National Aeronautics and Space Administration, , 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Elements of spacecraft design [[electronic resource] /] / Charles D. Brown
| Elements of spacecraft design [[electronic resource] /] / Charles D. Brown |
| Autore | Brown Charles D. <1930-> |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2002 |
| Descrizione fisica | 1 online resource |
| Disciplina | 629.47 |
| Collana | AIAA education series |
| Soggetto topico | Space vehicles - Design and construction |
| Soggetto genere / forma | Electronic books. |
| ISBN | 1-60086-051-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910454408103321 |
|
Brown Charles D. <1930->
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| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Elements of spacecraft design [[electronic resource] /] / Charles D. Brown
| Elements of spacecraft design [[electronic resource] /] / Charles D. Brown |
| Autore | Brown Charles D. <1930-> |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2002 |
| Descrizione fisica | 1 online resource |
| Disciplina | 629.47 |
| Collana | AIAA education series |
| Soggetto topico | Space vehicles - Design and construction |
| ISBN | 1-60086-051-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910782754303321 |
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Brown Charles D. <1930->
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| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Examining NASA's development on the space launch system and Orion crew capsule : hearing before the Subcommittee on Space and Aeronautics, Committee on Science, Space, and Technology, House of Representatives, One Hundred Twelfth Congress, second session, Wednesday, September 12, 2012
| Examining NASA's development on the space launch system and Orion crew capsule : hearing before the Subcommittee on Space and Aeronautics, Committee on Science, Space, and Technology, House of Representatives, One Hundred Twelfth Congress, second session, Wednesday, September 12, 2012 |
| Pubbl/distr/stampa | Washington : , : U.S. Government Printing Office, , 2012 |
| Descrizione fisica | 1 online resource (iii, 84 pages) : illustrations |
| Soggetto topico |
Launch vehicles (Astronautics) - United States - Design and construction
Space vehicles - Design and construction Launch vehicles (Astronautics) - Design and construction |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Examining NASA's Development on the Space Launch System and Orion Crew Capsule |
| Record Nr. | UNINA-9910708115103321 |
| Washington : , : U.S. Government Printing Office, , 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Exergy analysis and design optimization for aerospace vehicles and systems [[electronic resource] /] / edited by José A. Camberos, David J. Moorhouse
| Exergy analysis and design optimization for aerospace vehicles and systems [[electronic resource] /] / edited by José A. Camberos, David J. Moorhouse |
| Pubbl/distr/stampa | Reston, VA, : American Institute of Aeronautics and Astronautics, c2011 |
| Descrizione fisica | 1 online resource (658 p.) |
| Altri autori (Persone) |
CamberosJosé A
MoorhouseDavid J <1939-> (David John) |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Space vehicles - Design and construction
Space vehicles - Thermodynamics Aerospace engineering Exergy |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-840-1
1-60086-841-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Contents""; ""Preface""; ""Acknowledgments""; ""Nomenclature""; ""Chapter 1 Introduction""; ""Chapter 2 Fundamentals of Exergy Analysis""; ""Chapter 3 Applications of Exergy Analysis""; ""Chapter 4 Integrated Subsystem Analysis Using EntropyGeneration Minimization""; ""Chapter 5 Exergy-Based Design Methodology for Airfoil ShapeOptimization and Wing Analysis""; ""Chapter 6 Entropy Generation and Aerospace VehiclePerformance""; ""Chapter 7 Optimization Using Entropy-GenerationMinimization for Maximum Performance of Hypersonic Vehicles""
""Chapter 8 Characterization of Aerospace Vehicle Performanceand Mission Analysis Using Exergy""""Chapter 9 Mission-Integrated Synthesis and DesignOptimization (MIS/DO) of Aerospace Vehicles""; ""Chapter 10 MIS/DO Applied to High Performance AerospaceVehicles""; ""Chapter 11 Thermodynamics, Entropy GenerationMinimization, and the Constructal Law""; ""Chapter 12 Quantum Thermodynamics and the Modeling ofNonequilibrium Phenomena: Theory and Future Directions""; ""Chapter 13 Numerical Methods in Light of the Second Law""; ""Postlude""; ""Index""; ""Supporting Materials"" |
| Record Nr. | UNINA-9910462274703321 |
| Reston, VA, : American Institute of Aeronautics and Astronautics, c2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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