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Computational nonlinear mechanics in aerospace engineering [[electronic resource] /] / edited by Satya N. Atluri
| Computational nonlinear mechanics in aerospace engineering [[electronic resource] /] / edited by Satya N. Atluri |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1992 |
| Descrizione fisica | 1 online resource (563 p.) |
| Disciplina | 629.1/01515355 |
| Altri autori (Persone) | AtluriSatya N |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Aerodynamics - Mathematics
Airplanes - Materials - Mathematical models Nonlinear mechanics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-618-2
1-60086-399-X |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Table of Contents""; ""Chapter 1. Simplified Computational Methods for Elastic and Elastic-Plastic Fracture Problems""; ""Chapter 2. Field-Boundary Element Method for Nonlinear Solid Mechanics""; ""Chapter 3. Nonlinear Problems of Aeroelasticity""; ""Chapter 4. Finite Element Simulation of Compressible Flows with Shocks""; ""Chapter 5. Fast Projection Algorithm for Unstructured Meshes""; ""Chapter 6. Control of Numerical Diffusion in Computational Modeling of Vortex Flow""
""Chapter 7. Stochastic Computational Mechanics for Aerospace Structures""""Chapter 8. Boundary Integral Equation Methods for Aerodynamics""; ""Chapter 9. Theory and Implementation of High-Order Adaptive hp Methods for Analysis of Incompressible Viscous Flows""; ""Chapter 10. Probabilistic Evaluation of Uncertainties and Risks in Aerospace Components""; ""Chapter 11. Finite Element Computation of Incompressible Flows""; ""Chapter 12. Dynamic Response of Rapidly Heated Space Structures"" ""Chapter 13. Computation of Viscous Compressible Flows Using an Upwind Algorithm and Unstructured Meshes""""Chapter 14. Structural Optimization""; ""Chapter 15. Nonlinear Aeroelasticity and Chaos""; ""Author Index"" |
| Record Nr. | UNINA-9910457216503321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Computational nonlinear mechanics in aerospace engineering [[electronic resource] /] / edited by Satya N. Atluri
| Computational nonlinear mechanics in aerospace engineering [[electronic resource] /] / edited by Satya N. Atluri |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1992 |
| Descrizione fisica | 1 online resource (563 p.) |
| Disciplina | 629.1/01515355 |
| Altri autori (Persone) | AtluriSatya N |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Aerodynamics - Mathematics
Airplanes - Materials - Mathematical models Nonlinear mechanics |
| ISBN |
1-60086-618-2
1-60086-399-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Table of Contents""; ""Chapter 1. Simplified Computational Methods for Elastic and Elastic-Plastic Fracture Problems""; ""Chapter 2. Field-Boundary Element Method for Nonlinear Solid Mechanics""; ""Chapter 3. Nonlinear Problems of Aeroelasticity""; ""Chapter 4. Finite Element Simulation of Compressible Flows with Shocks""; ""Chapter 5. Fast Projection Algorithm for Unstructured Meshes""; ""Chapter 6. Control of Numerical Diffusion in Computational Modeling of Vortex Flow""
""Chapter 7. Stochastic Computational Mechanics for Aerospace Structures""""Chapter 8. Boundary Integral Equation Methods for Aerodynamics""; ""Chapter 9. Theory and Implementation of High-Order Adaptive hp Methods for Analysis of Incompressible Viscous Flows""; ""Chapter 10. Probabilistic Evaluation of Uncertainties and Risks in Aerospace Components""; ""Chapter 11. Finite Element Computation of Incompressible Flows""; ""Chapter 12. Dynamic Response of Rapidly Heated Space Structures"" ""Chapter 13. Computation of Viscous Compressible Flows Using an Upwind Algorithm and Unstructured Meshes""""Chapter 14. Structural Optimization""; ""Chapter 15. Nonlinear Aeroelasticity and Chaos""; ""Author Index"" |
| Record Nr. | UNINA-9910781411603321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Flight mechanics modeling and analysis / Jitendra R. Raol, Jatinder Singh
| Flight mechanics modeling and analysis / Jitendra R. Raol, Jatinder Singh |
| Autore | Raol, J. R. (Jitendra R.), 1947- |
| Pubbl/distr/stampa | Boca Raton : CRC Press, c2009 |
| Descrizione fisica | xx, 416 p. : ill. ; 25 cm |
| Disciplina | 629.132/30011 |
| Altri autori (Persone) | Singh, Jatinder, 1964-author |
| Soggetto topico |
Flight control - Simulation methods
Aerodynamics - Mathematics Airplanes - Control systems - Mathematical models |
| ISBN |
9781420067538 (hardback : alk. paper)
1420067532 (hardback : alk. paper) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991000933939707536 |
Raol, J. R. (Jitendra R.), 1947-
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| Boca Raton : CRC Press, c2009 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Salento | ||
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Modeling and simulation of aerospace vehicle dynamics [[electronic resource] /] / Peter H. Zipfel
| Modeling and simulation of aerospace vehicle dynamics [[electronic resource] /] / Peter H. Zipfel |
| Autore | Zipfel Peter H |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2007 |
| Descrizione fisica | xxii, 567 p. : ill |
| Disciplina | 629.132/30151 |
| Collana | AIAA education series |
| Soggetto topico |
Aerodynamics - Mathematics
Airplanes - Mathematical models Space vehicles - Dynamics - Mathematical models |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-090-7
1-60119-539-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910458385703321 |
|
Zipfel Peter H
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| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Modeling and simulation of aerospace vehicle dynamics [[electronic resource] /] / Peter H. Zipfel
| Modeling and simulation of aerospace vehicle dynamics [[electronic resource] /] / Peter H. Zipfel |
| Autore | Zipfel Peter H |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2007 |
| Descrizione fisica | xxii, 567 p. : ill |
| Disciplina | 629.132/30151 |
| Collana | AIAA education series |
| Soggetto topico |
Aerodynamics - Mathematics
Airplanes - Mathematical models Space vehicles - Dynamics - Mathematical models |
| ISBN |
1-60086-090-7
1-60119-539-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910784621403321 |
|
Zipfel Peter H
|
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| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Modeling and simulation of aerospace vehicle dynamics [[electronic resource] /] / Peter H. Zipfel
| Modeling and simulation of aerospace vehicle dynamics [[electronic resource] /] / Peter H. Zipfel |
| Autore | Zipfel Peter H |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2000 |
| Disciplina | 629.132/3/0151 |
| Collana |
AIAA education series Modeling and simulation of aerospace vehicle dynamics
AIAA education series |
| Soggetto topico |
Aerodynamics - Mathematics
Airplanes - Mathematical models Space vehicles - Dynamics - Mathematical models Space vehicles - Mathematical models - Dynamics Mechanical Engineering Engineering & Applied Sciences Aeronautics Engineering & Astronautics |
| Soggetto genere / forma | Electronic books. |
| ISBN | 1-60119-199-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9911004712603321 |
|
Zipfel Peter H
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| Reston, Va., : American Institute of Aeronautics and Astronautics, c2000 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Modeling of complex systems : application to aeronautical dynamics / / Emmanuel Grunn, Anh Tuan Pham
| Modeling of complex systems : application to aeronautical dynamics / / Emmanuel Grunn, Anh Tuan Pham |
| Autore | Grunn Emmanuel |
| Pubbl/distr/stampa | London ; ; Hoboken, New Jersey : , : ISTE : , : Wiley, , 2013 |
| Descrizione fisica | 1 online resource (124 p.) |
| Disciplina | 629.13230151 |
| Altri autori (Persone) | PhạmAnh Tuan (Engineer) |
| Collana | Automation-control and industrial engineering series |
| Soggetto topico |
Aerodynamics - Mathematics
System analysis - Mathematical models |
| ISBN |
1-118-57986-0
1-118-57997-6 1-118-58007-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title Page; Table of Contents; Introduction; Chapter 1. 0D Analytical Modeling of Airplane Motions; 1.1. References: axis systems on use; 1.1.1. Galilean reference: R0; 1.1.2. Airplane reference: RB (body) also called "linked reference"; 1.1.3. Resultant angular velocity; 1.2. Equations of motion of the airplane; 1.2.1. Expression of Newton's principle; 1.2.2. Expression of the dynamic momentum; 1.3. Description of external forces and torques; 1.3.1. Aerodynamic forces and torques; 1.3.2. Sign rules; 1.4. Description of aerodynamic coefficients; 1.4.1. Drag coefficient: Cx
1.4.2. Side lift coefficient: CY1.4.3. Vertical lift due to attack angle: CZα; 1.4.4. Lift due to pitch angular velocity: CZq; 1.4.5. Roll coefficients (due to β, δl , p); 1.4.6. Pitch coefficients (due to α, δm , q , static curvature); 1.4.7. Yaw coefficients (due to β, δn, r); 1.5. Aerodynamic data of a supersonic airliner for valuation of the software; 1.6. Horizontal flight as an initial condition; 1.7. Effect of gravitational forces; 1.8 calculation of the trajectory of the airplane in open space; 1.9. Validation by comparison with ONERA Concorde data 1.10. Definitions of aerodynamic coefficients and derivatives 1.10.1.1.10.1. Aerodynamic coefficients; 1.10.2. Total lift coefficient; 1.10.3. Drag characteristics: (dimensionless); 1.10.4. Side lift coefficient: CY (dimensionless); 1.10.5. Roll coefficients; 1.10.6. Pitch coefficients; 1.10.7. Yaw coefficients; Chapter 2. Design and Optimization of anUnmanned Aerial Vehicle (UAV); 2.1. General design of the drone; 2.2. Weight estimation; 2.3. Size estimation; 2.4. Mass and inertia evaluation; 2.4.1. Mass evaluation; 2.4.2. Measurement of the roll inertia (A) 2.4.3. Measurement of pitch inertia (B)2.4.4. Measurement of yaw inertia (C); 2.5. Convergence toward the target; Chapter 3. Organization of the Auto-Pilot; 3.1. Position of the drone in open space; 3.2. The Dog Law; 3.3. Flight tests; 3.4. Altitude control system; 3.5. Altitude measurement on an actual drone; Bibliography; Index |
| Record Nr. | UNINA-9910140187003321 |
|
Grunn Emmanuel
|
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| London ; ; Hoboken, New Jersey : , : ISTE : , : Wiley, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Modeling of complex systems : application to aeronautical dynamics / / Emmanuel Grunn, Anh Tuan Pham
| Modeling of complex systems : application to aeronautical dynamics / / Emmanuel Grunn, Anh Tuan Pham |
| Autore | Grunn Emmanuel |
| Pubbl/distr/stampa | London ; ; Hoboken, New Jersey : , : ISTE : , : Wiley, , 2013 |
| Descrizione fisica | 1 online resource (124 p.) |
| Disciplina | 629.13230151 |
| Altri autori (Persone) | PhạmAnh Tuan (Engineer) |
| Collana | Automation-control and industrial engineering series |
| Soggetto topico |
Aerodynamics - Mathematics
System analysis - Mathematical models |
| ISBN |
1-118-57986-0
1-118-57997-6 1-118-58007-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title Page; Table of Contents; Introduction; Chapter 1. 0D Analytical Modeling of Airplane Motions; 1.1. References: axis systems on use; 1.1.1. Galilean reference: R0; 1.1.2. Airplane reference: RB (body) also called "linked reference"; 1.1.3. Resultant angular velocity; 1.2. Equations of motion of the airplane; 1.2.1. Expression of Newton's principle; 1.2.2. Expression of the dynamic momentum; 1.3. Description of external forces and torques; 1.3.1. Aerodynamic forces and torques; 1.3.2. Sign rules; 1.4. Description of aerodynamic coefficients; 1.4.1. Drag coefficient: Cx
1.4.2. Side lift coefficient: CY1.4.3. Vertical lift due to attack angle: CZα; 1.4.4. Lift due to pitch angular velocity: CZq; 1.4.5. Roll coefficients (due to β, δl , p); 1.4.6. Pitch coefficients (due to α, δm , q , static curvature); 1.4.7. Yaw coefficients (due to β, δn, r); 1.5. Aerodynamic data of a supersonic airliner for valuation of the software; 1.6. Horizontal flight as an initial condition; 1.7. Effect of gravitational forces; 1.8 calculation of the trajectory of the airplane in open space; 1.9. Validation by comparison with ONERA Concorde data 1.10. Definitions of aerodynamic coefficients and derivatives 1.10.1.1.10.1. Aerodynamic coefficients; 1.10.2. Total lift coefficient; 1.10.3. Drag characteristics: (dimensionless); 1.10.4. Side lift coefficient: CY (dimensionless); 1.10.5. Roll coefficients; 1.10.6. Pitch coefficients; 1.10.7. Yaw coefficients; Chapter 2. Design and Optimization of anUnmanned Aerial Vehicle (UAV); 2.1. General design of the drone; 2.2. Weight estimation; 2.3. Size estimation; 2.4. Mass and inertia evaluation; 2.4.1. Mass evaluation; 2.4.2. Measurement of the roll inertia (A) 2.4.3. Measurement of pitch inertia (B)2.4.4. Measurement of yaw inertia (C); 2.5. Convergence toward the target; Chapter 3. Organization of the Auto-Pilot; 3.1. Position of the drone in open space; 3.2. The Dog Law; 3.3. Flight tests; 3.4. Altitude control system; 3.5. Altitude measurement on an actual drone; Bibliography; Index |
| Record Nr. | UNINA-9910820286703321 |
|
Grunn Emmanuel
|
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| London ; ; Hoboken, New Jersey : , : ISTE : , : Wiley, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
The simplifying assumptions, reducing the strict application of classical hydrodynamics to practical aeronautical computations / / by Max M. Munk
| The simplifying assumptions, reducing the strict application of classical hydrodynamics to practical aeronautical computations / / by Max M. Munk |
| Autore | Munk Max M (Max Michael), <1890-> |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1924 |
| Descrizione fisica | 1 online resource (16 pages) |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Hydrodynamics
Fluid dynamics Aerodynamics - Mathematics Viscosity |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713580803321 |
|
Munk Max M (Max Michael), <1890->
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| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1924 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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