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Aerodynamic principles of flight vehicles / / Argyris G. Panaras
| Aerodynamic principles of flight vehicles / / Argyris G. Panaras |
| Autore | Panaras A. G. |
| Pubbl/distr/stampa | Reston, Virginia : , : American Institute of Aeronautics and Astronautics, , [2012] |
| Descrizione fisica | 1 online resource (336 p.) |
| Disciplina | 629.132/3 |
| Collana | Library of flight |
| Soggetto topico |
Aerodynamics
High-speed aeronautics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-917-3
1-62870-155-2 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | ""Cover""; ""Title""; ""Copyright""; ""A Note from the Editor-in-Chief""; ""Table of Contents""; ""Preface""; ""Acknowledgements""; ""Chapter 1. Introduction""; ""Chapter 2. Vortices in Aerodynamics""; ""Chapter 3. Transonic and Supersonic Flows""; ""Chapter 4. Transonic Aircraft Configurations""; ""Chapter 5. High-Supersonic/Hypersonic Flows""; ""Appendix: Analysis of Fundamental Relations and Theorems""; ""Index""; ""Supporting Materials"" |
| Record Nr. | UNINA-9910458283903321 |
Panaras A. G.
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| Reston, Virginia : , : American Institute of Aeronautics and Astronautics, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerodynamic principles of flight vehicles / / Argyris G. Panaras
| Aerodynamic principles of flight vehicles / / Argyris G. Panaras |
| Autore | Panaras A. G. |
| Pubbl/distr/stampa | Reston, Virginia : , : American Institute of Aeronautics and Astronautics, , [2012] |
| Descrizione fisica | 1 online resource (336 p.) |
| Disciplina | 629.132/3 |
| Collana | Library of flight |
| Soggetto topico |
Aerodynamics
High-speed aeronautics |
| ISBN |
1-60086-917-3
1-62870-155-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | ""Cover""; ""Title""; ""Copyright""; ""A Note from the Editor-in-Chief""; ""Table of Contents""; ""Preface""; ""Acknowledgements""; ""Chapter 1. Introduction""; ""Chapter 2. Vortices in Aerodynamics""; ""Chapter 3. Transonic and Supersonic Flows""; ""Chapter 4. Transonic Aircraft Configurations""; ""Chapter 5. High-Supersonic/Hypersonic Flows""; ""Appendix: Analysis of Fundamental Relations and Theorems""; ""Index""; ""Supporting Materials"" |
| Record Nr. | UNINA-9910790901603321 |
|
Panaras A. G.
|
||
| Reston, Virginia : , : American Institute of Aeronautics and Astronautics, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerodynamic principles of flight vehicles / / Argyris G. Panaras
| Aerodynamic principles of flight vehicles / / Argyris G. Panaras |
| Autore | Panaras A. G. |
| Pubbl/distr/stampa | Reston, Virginia : , : American Institute of Aeronautics and Astronautics, , [2012] |
| Descrizione fisica | 1 online resource (336 p.) |
| Disciplina | 629.132/3 |
| Collana | Library of flight |
| Soggetto topico |
Aerodynamics
High-speed aeronautics |
| ISBN |
1-60086-917-3
1-62870-155-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | ""Cover""; ""Title""; ""Copyright""; ""A Note from the Editor-in-Chief""; ""Table of Contents""; ""Preface""; ""Acknowledgements""; ""Chapter 1. Introduction""; ""Chapter 2. Vortices in Aerodynamics""; ""Chapter 3. Transonic and Supersonic Flows""; ""Chapter 4. Transonic Aircraft Configurations""; ""Chapter 5. High-Supersonic/Hypersonic Flows""; ""Appendix: Analysis of Fundamental Relations and Theorems""; ""Index""; ""Supporting Materials"" |
| Record Nr. | UNINA-9910828437003321 |
|
Panaras A. G.
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||
| Reston, Virginia : , : American Institute of Aeronautics and Astronautics, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
| Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham |
| Autore | Durham Wayne <1941-> |
| Pubbl/distr/stampa | Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 |
| Descrizione fisica | 1 online resource (308 p.) |
| Disciplina | 629.132/3 |
| Collana | Aerospace series |
| Soggetto topico |
Aerodynamics
Flight Flight control Airplanes - Performance |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-118-64680-0
1-118-64679-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title Page; Copyright; Contents; Series Preface; Glossary; Chapter 1 Introduction; 1.1 Background; 1.2 Overview; 1.3 Customs and Conventions; References; Chapter 2 Coordinate Systems; 2.1 Background; 2.2 The Coordinate Systems; 2.2.1 The inertial reference frame, FI; 2.2.2 The earth-centered reference frame, FEC; 2.2.3 The earth-fixed reference frame, FE; 2.2.4 The local-horizontal reference frame, FH; 2.2.5 Body-fixed reference frames, FB; 2.2.6 Wind-axis system, FW; 2.2.7 Atmospheric reference frame; 2.3 Vector Notation; 2.4 Customs and Conventions; 2.4.1 Latitude and longitude
2.4.2 Body axes2.4.3 `The' body-axis system; 2.4.4 Aerodynamic angles; Problems; References; Chapter 3 Coordinate System Transformations; 3.1 Problem Statement; 3.2 Transformations; 3.2.1 Definitions; 3.2.2 Direction cosines; 3.2.3 Euler angles; 3.2.4 Euler parameters; 3.3 Transformations of Systems of Equations; 3.4 Customs and Conventions; 3.4.1 Names of Euler angles; 3.4.2 Principal values of Euler angles; Problems; Reference; Chapter 4 Rotating Coordinate Systems; 4.1 General; 4.2 Direction Cosines; 4.3 Euler Angles; 4.4 Euler Parameters; 4.5 Customs and Conventions 4.5.1 Angular velocity componentsProblems; Chapter 5 Inertial Accelerations; 5.1 General; 5.2 Inertial Acceleration of a Point; 5.2.1 Arbitrary moving reference frame; 5.2.2 Earth-centered moving reference frame; 5.2.3 Earth-fixed moving reference frame; 5.3 Inertial Acceleration of a Mass; 5.3.1 Linear acceleration; 5.3.2 Rotational acceleration; 5.4 States; 5.5 Customs and Conventions; 5.5.1 Linear velocity components; 5.5.2 Angular velocity components; 5.5.3 Forces; 5.5.4 Moments; 5.5.5 Groupings; Problems; Chapter 6 Forces and Moments; 6.1 General; 6.1.1 Assumptions; 6.1.2 State variables 6.1.3 State rates6.1.4 Flight controls; 6.1.5 Independent variables; 6.2 Non-Dimensionalization; 6.3 Non-Dimensional Coefficient Dependencies; 6.3.1 General; 6.3.2 Altitude dependencies; 6.3.3 Velocity dependencies; 6.3.4 Angle-of-attack dependencies; 6.3.5 Sideslip dependencies; 6.3.6 Angular velocity dependencies; 6.3.7 Control dependencies; 6.3.8 Summary of dependencies; 6.4 The Linear Assumption; 6.5 Tabular Data; 6.6 Customs and Conventions; Problems; Chapter 7 Equations of Motion; 7.1 General; 7.2 Body-Axis Equations; 7.2.1 Body-axis force equations; 7.2.2 Body-axis moment equations 7.2.3 Body-axis orientation equations (kinematic equations)7.2.4 Body-axis navigation equations; 7.3 Wind-Axis Equations; 7.3.1 Wind-axis force equations; 7.3.2 Wind-axis orientation equations (kinematic equations); 7.3.3 Wind-axis navigation equations; 7.4 Steady-State Solutions; 7.4.1 General; 7.4.2 Special cases; 7.4.3 The trim problem; Problems; Reference; Chapter 8 Linearization; 8.1 General; 8.2 Taylor Series; 8.3 Nonlinear Ordinary Differential Equations; 8.4 Systems of Equations; 8.5 Examples; 8.5.1 General; 8.5.2 A kinematic equation; 8.5.3 A moment equation; 8.5.4 A force equation 8.6 Customs and Conventions |
| Record Nr. | UNINA-9910463787503321 |
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Durham Wayne <1941->
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| Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
| Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham |
| Autore | Durham Wayne <1941-> |
| Pubbl/distr/stampa | Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 |
| Descrizione fisica | xix, 286 p. : ill |
| Disciplina | 629.132/3 |
| Collana | Aerospace series |
| Soggetto topico |
Aerodynamics
Airplanes - Performance Flight control Flight |
| ISBN |
9781118646793
1118646797 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910796091203321 |
|
Durham Wayne <1941->
|
||
| Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham
| Aircraft flight dynamics and control [[electronic resource] /] / Wayne Durham |
| Autore | Durham Wayne <1941-> |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 |
| Descrizione fisica | xix, 286 p. : ill |
| Disciplina | 629.132/3 |
| Collana | Aerospace series |
| Soggetto topico |
Aerodynamics
Airplanes - Performance Flight control Flight |
| ISBN |
9781118646793
1118646797 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover -- Title Page -- Copyright -- Contents -- Series Preface -- Glossary -- Chapter 1 Introduction -- 1.1 Background -- 1.2 Overview -- 1.3 Customs and Conventions -- References -- Chapter 2 Coordinate Systems -- 2.1 Background -- 2.2 The Coordinate Systems -- 2.2.1 The inertial reference frame, FI -- 2.2.2 The earth-centered reference frame, FEC -- 2.2.3 The earth-fixed reference frame, FE -- 2.2.4 The local-horizontal reference frame, FH -- 2.2.5 Body-fixed reference frames, FB -- 2.2.6 Wind-axis system, FW -- 2.2.7 Atmospheric reference frame -- 2.3 Vector Notation -- 2.4 Customs and Conventions -- 2.4.1 Latitude and longitude -- 2.4.2 Body axes -- 2.4.3 `The' body-axis system -- 2.4.4 Aerodynamic angles -- Problems -- References -- Chapter 3 Coordinate System Transformations -- 3.1 Problem Statement -- 3.2 Transformations -- 3.2.1 Definitions -- 3.2.2 Direction cosines -- 3.2.3 Euler angles -- 3.2.4 Euler parameters -- 3.3 Transformations of Systems of Equations -- 3.4 Customs and Conventions -- 3.4.1 Names of Euler angles -- 3.4.2 Principal values of Euler angles -- Problems -- Reference -- Chapter 4 Rotating Coordinate Systems -- 4.1 General -- 4.2 Direction Cosines -- 4.3 Euler Angles -- 4.4 Euler Parameters -- 4.5 Customs and Conventions -- 4.5.1 Angular velocity components -- Problems -- Chapter 5 Inertial Accelerations -- 5.1 General -- 5.2 Inertial Acceleration of a Point -- 5.2.1 Arbitrary moving reference frame -- 5.2.2 Earth-centered moving reference frame -- 5.2.3 Earth-fixed moving reference frame -- 5.3 Inertial Acceleration of a Mass -- 5.3.1 Linear acceleration -- 5.3.2 Rotational acceleration -- 5.4 States -- 5.5 Customs and Conventions -- 5.5.1 Linear velocity components -- 5.5.2 Angular velocity components -- 5.5.3 Forces -- 5.5.4 Moments -- 5.5.5 Groupings -- Problems -- Chapter 6 Forces and Moments -- 6.1 General.
6.1.1 Assumptions -- 6.1.2 State variables -- 6.1.3 State rates -- 6.1.4 Flight controls -- 6.1.5 Independent variables -- 6.2 Non-Dimensionalization -- 6.3 Non-Dimensional Coefficient Dependencies -- 6.3.1 General -- 6.3.2 Altitude dependencies -- 6.3.3 Velocity dependencies -- 6.3.4 Angle-of-attack dependencies -- 6.3.5 Sideslip dependencies -- 6.3.6 Angular velocity dependencies -- 6.3.7 Control dependencies -- 6.3.8 Summary of dependencies -- 6.4 The Linear Assumption -- 6.5 Tabular Data -- 6.6 Customs and Conventions -- Problems -- Chapter 7 Equations of Motion -- 7.1 General -- 7.2 Body-Axis Equations -- 7.2.1 Body-axis force equations -- 7.2.2 Body-axis moment equations -- 7.2.3 Body-axis orientation equations (kinematic equations) -- 7.2.4 Body-axis navigation equations -- 7.3 Wind-Axis Equations -- 7.3.1 Wind-axis force equations -- 7.3.2 Wind-axis orientation equations (kinematic equations) -- 7.3.3 Wind-axis navigation equations -- 7.4 Steady-State Solutions -- 7.4.1 General -- 7.4.2 Special cases -- 7.4.3 The trim problem -- Problems -- Reference -- Chapter 8 Linearization -- 8.1 General -- 8.2 Taylor Series -- 8.3 Nonlinear Ordinary Differential Equations -- 8.4 Systems of Equations -- 8.5 Examples -- 8.5.1 General -- 8.5.2 A kinematic equation -- 8.5.3 A moment equation -- 8.5.4 A force equation -- 8.6 Customs and Conventions -- 8.6.1 Omission of -- 8.6.2 Dimensional derivatives -- 8.6.3 Added mass -- 8.7 The Linear Equations -- 8.7.1 Linear equations -- 8.7.2 Matrix forms of the linear equations -- Problems -- References -- Chapter 9 Solutions to the Linear Equations -- 9.1 Scalar Equations -- 9.2 Matrix Equations -- 9.3 Initial Condition Response -- 9.3.1 Modal analysis -- 9.4 Mode Sensitivity and Approximations -- 9.4.1 Mode sensitivity -- 9.4.2 Approximations -- 9.5 Forced Response -- 9.5.1 Transfer functions. 9.5.2 Steady-state response -- Problems -- Chapter 10 Aircraft Flight Dynamics -- 10.1 Example: Longitudinal Dynamics -- 10.1.1 System matrices -- 10.1.2 State transition matrix and eigenvalues -- 10.1.3 Eigenvector analysis -- 10.1.4 Longitudinal mode sensitivity and approximations -- 10.1.5 Forced response -- 10.2 Example: Lateral-Directional Dynamics -- 10.2.1 System matrices -- 10.2.2 State transition matrix and eigenvalues -- 10.2.3 Eigenvector analysis -- 10.2.4 Lateral-directional mode sensitivity and approximations -- 10.2.5 Forced response -- Problems -- References -- Chapter 11 Flying Qualities -- 11.1 General -- 11.1.1 Method -- 11.1.2 Specifications and standards -- 11.2 MIL-F-8785C Requirements -- 11.2.1 General -- 11.2.2 Longitudinal flying qualities -- 11.2.3 Lateral-directional flying qualitities -- Problems -- References -- Chapter 12 Automatic Flight Control -- 12.1 Simple Feedback Systems -- 12.1.1 First-order systems -- 12.1.2 Second-order systems -- 12.1.3 A general representation -- 12.2 Example Feedback Control Applications -- 12.2.1 Roll mode -- 12.2.2 Short-period mode -- 12.2.3 Phugoid -- 12.2.4 Coupled roll-spiral oscillation -- Problems -- References -- Chapter 13 Trends in Automatic Flight Control -- 13.1 Overview -- 13.2 Dynamic Inversion -- 13.2.1 The controlled equations -- 13.2.2 The kinematic equations -- 13.2.3 The complementary equations -- 13.3 Control Allocation -- 13.3.1 Background -- 13.3.2 Problem statement -- 13.3.3 Optimality -- 13.3.4 Sub-optimal solutions -- 13.3.5 Optimal solutions -- 13.3.6 Near-optimal solutions -- Problems -- References -- Appendix A Example Aircraft -- Reference -- Appendix B Linearization -- B.1 Derivation of Frequently Used Derivatives -- B.2 Non-dimensionalization of the Rolling Moment Equation -- B.3 Body Axis Z-Force and Thrust Derivatives. B.4 Non-dimensionalization of the Z-Force Equation -- Appendix C Derivation of Euler Parameters -- Appendix D Fedeeva's Algorithm -- Reference -- Appendix E MATLAB® Commands Used in the Text -- E.1 Using MATLAB® -- E.2 Eigenvalues and Eigenvectors -- E.3 State-Space Representation -- E.4 Transfer Function Representation -- E.5 Root Locus -- E.6 MATLAB® Functions (m-files) -- E.6.1 Example aircraft -- E.6.2 Mode sensitivity matrix -- E.6.3 Cut-and-try root locus gains -- E.7 Miscellaneous Applications and Notes -- E.7.1 Matrices -- E.7.2 Commands used to create Figures 10.2 and 10.3 -- Index. |
| Record Nr. | UNINA-9910814647003321 |
|
Durham Wayne <1941->
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| Chichester, West Sussex, : John Wiley & Sons, Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Applied computational aerodynamics [[electronic resource] /] / edited by P.A. Henne
| Applied computational aerodynamics [[electronic resource] /] / edited by P.A. Henne |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., c1990 |
| Descrizione fisica | 1 online resource (926 p.) |
| Disciplina |
629.1 s
629.132/3 |
| Altri autori (Persone) | HenneP. A |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Aerodynamics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-598-4
1-60086-379-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 2. History -- pt. 2. Computational aerodynamic schemes -- pt. 3. Airfoils, wings, and wing bodies -- pt. 4. High-lift systems -- pt. 5. Propulsion -- pt. 6. Rotors -- pt. 7. Complex configurations -- pt. 8. Forecast. |
| Record Nr. | UNINA-9910457215603321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., c1990 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Applied computational aerodynamics [[electronic resource] /] / edited by P.A. Henne
| Applied computational aerodynamics [[electronic resource] /] / edited by P.A. Henne |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., c1990 |
| Descrizione fisica | 1 online resource (926 p.) |
| Disciplina |
629.1 s
629.132/3 |
| Altri autori (Persone) | HenneP. A |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Aerodynamics |
| ISBN |
1-60086-598-4
1-60086-379-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 2. History -- pt. 2. Computational aerodynamic schemes -- pt. 3. Airfoils, wings, and wing bodies -- pt. 4. High-lift systems -- pt. 5. Propulsion -- pt. 6. Rotors -- pt. 7. Complex configurations -- pt. 8. Forecast. |
| Record Nr. | UNINA-9910781402903321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., c1990 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Applied computational aerodynamics [[electronic resource] /] / edited by P.A. Henne
| Applied computational aerodynamics [[electronic resource] /] / edited by P.A. Henne |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., c1990 |
| Descrizione fisica | 1 online resource (926 p.) |
| Disciplina |
629.1 s
629.132/3 |
| Altri autori (Persone) | HenneP. A |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Aerodynamics |
| ISBN |
1-60086-598-4
1-60086-379-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 2. History -- pt. 2. Computational aerodynamic schemes -- pt. 3. Airfoils, wings, and wing bodies -- pt. 4. High-lift systems -- pt. 5. Propulsion -- pt. 6. Rotors -- pt. 7. Complex configurations -- pt. 8. Forecast. |
| Record Nr. | UNINA-9910817254903321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., c1990 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Flight vehicle performance and aerodynamic control [[electronic resource] /] / Frederick O. Smetana
| Flight vehicle performance and aerodynamic control [[electronic resource] /] / Frederick O. Smetana |
| Autore | Smetana Frederick O. <1928-> |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2001 |
| Descrizione fisica | 1 online resource (380 p.) |
| Disciplina | 629.132/3 |
| Collana | AIAA education series |
| Soggetto topico |
Airplanes - Performance
Airplanes - Control surfaces Aerodynamics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-185-7
1-60086-057-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Why Another Performance Book?""; ""The Included Software""; ""Chapter 1. Basic Nomenclature""; ""Chapter 2. The Atmosphere""; ""Chapter 3. Characteristics of Power Plants""; ""Chapter 4. Flight Vehicle Lift-Drag Characteristics""; ""Chapter 5. Equations of Motion""; ""Chapter 6. Determination of Aerodynamic Characteristics""; ""Chapter 7. Flight Vehicle Performance""; ""Chapter 8. Aerodynamic Control Forces and Static Stability""; ""Chapter 9. Flight Vehicle Aerodynamic Control""
""Appendix A. Pressure, Density, and Temperature Variations with Altitude""""Appendix B. Octane Ratings""; ""Appendix C. Description and Use of Program TRAJECT""; ""Glossary""; ""References""; ""Subject Index"" |
| Record Nr. | UNINA-9910457212003321 |
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Smetana Frederick O. <1928->
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| Reston, Va., : American Institute of Aeronautics and Astronautics, c2001 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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