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Evaluation of U.S. Air Force preacquisition technology development / / National Research Council of the National Academies
| Evaluation of U.S. Air Force preacquisition technology development / / National Research Council of the National Academies |
| Pubbl/distr/stampa | Washington, D.C., : National Academies Press, 2011 |
| Descrizione fisica | 1 online resource (155 p.) |
| Disciplina | 629.1 |
| Soggetto topico | Aeronautics, Military - Technological innovations - United States |
| ISBN |
0-309-20997-8
1-283-01917-5 9786613019172 0-309-16276-9 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Front Matter""; ""Preface""; ""Acknowledgment of Reviewers""; ""Contents""; ""Acronyms""; ""Summary""; ""1 Preacquisition Technology Development for Air Force Weapon Systems""; ""2 The Current State of the Air Force's Acquisition Policies, Processes, and Workforce""; ""3 Government and Industry Best Practices""; ""4 The Recommended Path Forward""; ""Appendixes""; ""Appendix A: Biographical Sketches of Committee Members""; ""Appendix B: Meetings and Participating Organizations""; ""Appendix C: Background Information on Policies and Processes Related to Technology Development""
""Appendix D: Background Information on the Vanguard Process and Applied Technology Councils"" |
| Record Nr. | UNINA-9910812263303321 |
| Washington, D.C., : National Academies Press, 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Evolution of motions of a rigid body about its center of mass [[electronic resource] /] / by Felix L. Chernousko, Leonid D. Akulenko, Dmytro D. Leshchenko
| Evolution of motions of a rigid body about its center of mass [[electronic resource] /] / by Felix L. Chernousko, Leonid D. Akulenko, Dmytro D. Leshchenko |
| Autore | Chernousko Felix L |
| Edizione | [1st ed. 2017.] |
| Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2017 |
| Descrizione fisica | 1 online resource (XXXVIII, 241 p. 52 illus.) |
| Disciplina | 629.1 |
| Soggetto topico |
Aerospace engineering
Astronautics Mathematical physics Mechanics Aerospace Technology and Astronautics Mathematical Physics Classical Mechanics |
| ISBN | 3-319-53928-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | The foundations of dynamics of a rigid body with a fixed point -- Motion of a rigid body by inertia. Euler's case -- Lagrange's case -- Equations of perturbed motion of a rigid body about its center of mass -- Perturbation torques acting upon a rigid body -- Motion of a satellite about its center of mass under the action of gravitational torque -- Motion of a rigid body with a cavity filled with a viscous fluid -- Evolution of rotations of a rigid body in a medium -- Motion of a rigid body with internal degrees of freedom -- Influence of the torque due to the solar pressure upon the motion of a Sun satellite relative to its center of mass -- Perturbed motions of a rigid body close to Lagrange's case. |
| Record Nr. | UNINA-9910254322803321 |
Chernousko Felix L
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| Cham : , : Springer International Publishing : , : Imprint : Springer, , 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental Techniques, Rotating Machinery, and Acoustics, Volume 8 [[electronic resource] ] : Proceedings of the 33rd IMAC, A Conference and Exposition on Structural Dynamics, 2015 / / edited by James De Clerck
| Experimental Techniques, Rotating Machinery, and Acoustics, Volume 8 [[electronic resource] ] : Proceedings of the 33rd IMAC, A Conference and Exposition on Structural Dynamics, 2015 / / edited by James De Clerck |
| Edizione | [1st ed. 2015.] |
| Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2015 |
| Descrizione fisica | 1 online resource (275 p.) |
| Disciplina |
620
620.1 629.1 |
| Collana | Conference Proceedings of the Society for Experimental Mechanics Series |
| Soggetto topico |
Vibration
Dynamical systems Dynamics Aerospace engineering Astronautics Mechanics Mechanics, Applied Vibration, Dynamical Systems, Control Aerospace Technology and Astronautics Solid Mechanics |
| ISBN | 3-319-15236-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 1. A Computational Model to Investigate the Influence of Spacing Errors on Spur Gear Pair Dynamics -- 2. Drill Vibration Suppression through Phase-Locked Loop Control -- 3. Towards the Selection of Balancing Planes to Attain Low Vibrations in Flexible Rotor Motor Systems -- 4. Experimental Acoustic Modal Analysis of an Automotive Cabin -- 5. Uncorrelated Noise Sources Separation Using Inverse Beamforming -- 6. ACTIVE NOISE CONTROL EXPERIMENT MINIMISING RADIATION OF ACTIVE ENERGY -- 7. Active Control of Transformer Noise by MIMO Algorithm -- 8. Numerical Prediction Tools for Low-frequency Sound Insulation in Lightweight Buildings -- 9. Reduction of Radiating Sound from CFRP Laminated Plates with Orthotropy -- 10. Rotating disc model for complex eigenvalue analysis of brake squeal -- 11. Validation of closed-loop coupling disc brake model for squeal analysis -- 12. Estimation of Torsional Compliance from Free-Free FRF Measurements: eRCF Theory -- 13. An Estimation of Torsional Compliance (Stiffness) from Free-Free FRF Measurements: eRCF Application -- 14. Estimation of Bending Compliance (Stiffness) from Free-Free FRF Measurements: eBCF Theory -- 15. In-Situ Experimental Modal Analysis of a Direct-Drive Wind Turbine Generator -- 16. Effect of Radial Confinement on Wave Propagation and Vibrational Response in Bars -- 17. Component Qualification Using 3D Laser Vibrometry and Transmissibility Models -- 18. Exploiting Continuous Scanning Laser Doppler Vibrometry and Wavelet Processing for Damage Detection -- 19. Use of 3D Scanning Laser Vibrometer for Full Field Strain Measurements -- 20. Inline measurements of rail bending and torsion through a portable device -- 21. Forty Years of Use and Abuse of Impact Testing: A Practical Guide to Making Good FRF Measurements -- 22. Detection of Coupling Misalignment by Extended Orbits -- 23. Linear and Nonlinear Response of a Rectangular Plate Measured with Continuous-Scan Laser Doppler Vibrometry and 3D-Digital Image Correlation -- 24. Vibration Event Localization in an Instrumented Building -- 25. Loading Effect on Induction Motor Eccentricity Diagnostics Using Vibration and Motor Current. |
| Record Nr. | UNINA-9910299839503321 |
| Cham : , : Springer International Publishing : , : Imprint : Springer, , 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Failure Characteristics Analysis and Fault Diagnosis for Liquid Rocket Engines [[electronic resource] /] / by Wei Zhang
| Failure Characteristics Analysis and Fault Diagnosis for Liquid Rocket Engines [[electronic resource] /] / by Wei Zhang |
| Autore | Zhang Wei |
| Edizione | [1st ed. 2016.] |
| Pubbl/distr/stampa | Berlin, Heidelberg : , : Springer Berlin Heidelberg : , : Imprint : Springer, , 2016 |
| Descrizione fisica | 1 online resource (XIV, 401 p. 153 illus., 61 illus. in color.) |
| Disciplina | 629.1 |
| Soggetto topico |
Aerospace engineering
Astronautics Computational intelligence Application software Aerospace Technology and Astronautics Computational Intelligence Computer Applications |
| ISBN | 3-662-49254-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- Failure pattern and corresponding mechanism analysis of liquid Rocket engines (LRE) -- Analysis method of failure model for LRE -- Failure characteristics analysis of LRE -- Fault diagnosis of LRE based on artificial neural net -- Fault diagnosis method based on Wavelet transform -- Fault diagnosis method based on artificial immune system -- Fault diagnosis method based on fuzzy theory -- Fault analysis and diagnosis method based on statistical learning theory -- Fault diagnosis method based on hide Markov model -- Fault prediction method of LRE. |
| Record Nr. | UNINA-9910254227703321 |
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Zhang Wei
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| Berlin, Heidelberg : , : Springer Berlin Heidelberg : , : Imprint : Springer, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components [[electronic resource] /] / by Russell Wanhill, Simon Barter, Loris Molent
| Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components [[electronic resource] /] / by Russell Wanhill, Simon Barter, Loris Molent |
| Autore | Wanhill Russell |
| Edizione | [1st ed. 2019.] |
| Pubbl/distr/stampa | Dordrecht : , : Springer Netherlands : , : Imprint : Springer, , 2019 |
| Descrizione fisica | 1 online resource (XI, 99 p. 50 illus., 47 illus. in color.) |
| Disciplina | 629.1 |
| Collana | SpringerBriefs in Applied Sciences and Technology |
| Soggetto topico |
Aerospace engineering
Astronautics Mechanics Mechanics, Applied Structural materials Aerospace Technology and Astronautics Solid Mechanics Structural Materials |
| ISBN | 94-024-1675-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 1 Historical Review -- 1.1 FCG Parameters, Concepts and Testing -- 1.2 FCG ‘Laws’ and Models -- 1.3 Summary -- 2 Basic Information for Aircraft FCG Failure and Lifing Analyses -- 2.1 Importance of Fatigue for Aircraft Structural Failures -- 2.2 Fatigue Crack Nucleation, Discontinuities, Early FCG and Damage Tolerance -- 2.3 Summary of FCG Lifing Methods -- 3 Quantitative Fractography (QF) for FCG analyses -- 3.1 Introduction -- 3.2 Fatigue Striation FCG Analyses -- 3.3 Progression Marking FCG Analyses -- 3.4 Fatigue-nucleating Discontinuities and Equivalent Pre-crack Sizes (EPS) -- 3.5 QF Techniques for Fatigue Fracture Surfaces -- 3.6 A Cautionary Note -- 4 Aermacchi MB-326H Wing Spar (1990): Exponential FCG Analysis -- 4.1 Introduction -- 4.2 FCG Analysis for the Failed Spar -- 4.3 Further Examination of Wing Spars -- 4.4 Lessons Learned -- 5 P&W 125B Engine Bearing (1994): 2-Stage Exponential FCG Analysis -- 5.1 Introduction -- 5.2 The Failed No.3 Bearing: Macroscopic and |Metallographic Examination -- 5.3 Cage Failure and FCG Analysis -- 5.4 Interpretation of the Results, Conclusions, and Remedial Action -- 6. EBA Example Lifing Assessment (2004): F/A-18 Horizontal StabilatorSpindles -- 6.1 Introduction -- 6.2 EBA Validation for the F/A-18 Horizontal Stabilator Spindles -- 6.3 EBA and Total Life Assessment for the F/A-18 Horizontal Stabilator Spindles -- 7. LCFLF Example Lifing Assessment (2004): F/A-18 Vertical Tail Attachment Stubs -- 7.1 Introduction -- 7.2 The FT46 Stub Flange Crack -- 7.3 Fractography of the FT46 Stub Flange Crack -- 7.4 LCFLF Life Assessment for the FT46 Stub Flange Crack -- 8. Cubic Rule Life Prediction Examples -- 8.1 Introduction -- 8.2 McDonnell Douglas F4E Spectrum Coupon Test Data -- 8.3 Lockheed Martin P3C Spectrum Coupon Test Data -- 8.4 Summary -- 9. Fokker 100 Fuselage Test: Lap Joints Exponential FCG Analysis -- 9.1 Introduction -- 9.2 FCG Analysis of the Cracked Lap Splice [71.72.95] -- 10. Sikorsky S-61N Rotor Blade (1974): Exponential FCGR Analysis -- 10.1 Introduction -- 10.2 FCG Analysis for the Crashed Helicopter -- 10.3 Prediction of Detectable FCG Lives -- 10.4 Results and Remedial Actions (Lessons Learned) -- 11. Westland Lynx Rotor Hub (1998): Progression Marking LEFM Analysis -- 11.1 Introduction -- 11.2 Fractography of Early Fatigue Cracking in the M326 Yellow Arm -- 11.3 Fractography of Early Fatigue Cracking in the M6 Arm and M326Specimens -- 11.4 FRTB + LEFM Estimations of Damaging Service Fatigue Stress Levels -- 11.5 Measurements of Service Loads and Fatigue Analysis by GKNW -- 11.6 Causes of Failure and Remedial Action -- 12. Closing Remarks -- References. |
| Record Nr. | UNINA-9910337636903321 |
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Wanhill Russell
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| Dordrecht : , : Springer Netherlands : , : Imprint : Springer, , 2019 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flexible Engineering Toward Green Aircraft [[electronic resource] ] : CAE Tools for Sustainable Mobility / / edited by Marco Evangelos Biancolini, Ubaldo Cella
| Flexible Engineering Toward Green Aircraft [[electronic resource] ] : CAE Tools for Sustainable Mobility / / edited by Marco Evangelos Biancolini, Ubaldo Cella |
| Edizione | [1st ed. 2020.] |
| Pubbl/distr/stampa | Cham : , : Springer International Publishing : , : Imprint : Springer, , 2020 |
| Descrizione fisica | 1 online resource (XII, 187 p. 130 illus., 77 illus. in color.) |
| Disciplina | 629.1 |
| Collana | Lecture Notes in Applied and Computational Mechanics |
| Soggetto topico |
Fluids
Aerospace engineering Astronautics Transportation Politics and war Sustainable development Fluid- and Aerodynamics Aerospace Technology and Astronautics Military and Defence Studies Sustainable Development |
| ISBN | 3-030-36514-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | The next generation of aircraft -- Aeroelastic wind tunnel tests of the RIBES wing model -- Validation of high fidelity computational methods for aeronautical FSI analyses -- High-fidelity static aeroelastic simulations of the Common Research Model -- Aero-elastic simulations using the NSMB CFD solver including results for a Strut Braced Wing -- Semi-analytical modeling of non-stationary fluid-structure interaction -- Fluid structure modelling of ground induced vibrations by mesh morphing and modal superposition -- Unsteady FSI Analysis of a Square Array of Tubes in Water Crossflow -- Risk measures applied to robust aerodynamic shape design optimization -- Aero-structural Optimization of a MALE configuration in the AGILE MDO Framework. |
| Record Nr. | UNINA-9910383840803321 |
| Cham : , : Springer International Publishing : , : Imprint : Springer, , 2020 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flight dynamics / Robert F. Stengel
| Flight dynamics / Robert F. Stengel |
| Autore | Stengel, Robert F. |
| Pubbl/distr/stampa | Princeton, NJ : Princeton University Press, c2004 |
| Descrizione fisica | xviii, 845 p. : ill. ; 24 cm |
| Disciplina | 629.1 |
| Soggetto topico |
Aerodynamics
Flight Airplanes - Performance |
| ISBN | 0691114072 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991001427319707536 |
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Stengel, Robert F.
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| Princeton, NJ : Princeton University Press, c2004 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Salento | ||
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Flight dynamics principles [[electronic resource] ] : [a linear systems approach to aircraft stability and control] / / M.V. Cook
| Flight dynamics principles [[electronic resource] ] : [a linear systems approach to aircraft stability and control] / / M.V. Cook |
| Autore | Cook M. V |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 |
| Descrizione fisica | 1 online resource (491 p.) |
| Disciplina |
629.1
629.1323 |
| Collana | Elsevier aerospace engineering series |
| Soggetto topico | Aerodynamics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-281-02927-0
9786611029272 0-08-055036-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front cover; Flight Dynamics Principles; Copyright page; Contents; Preface to the first edition; Preface to the second edition; Acknowledgements; Nomenclature; Chapter 1. Introduction; 1.1 Overview; 1.2 Flying and handling qualities; 1.3 General considerations; 1.4 Aircraft equations of motion; 1.5 Aerodynamics; 1.6 Computers; 1.7 Summary; References; Chapter 2. Systems of axes and notation; 2.1 Earth axes; 2.2 Aircraft body fixed axes; 2.3 Euler angles and aircraft attitude; 2.4 Axes transformations; 2.5 Aircraft reference geometry; 2.6 Controls notation; 2.7 Aerodynamic reference centres
ReferencesProblems; Chapter 3. Static equilibrium and trim; 3.1 Trim equilibrium; 3.2 The pitching moment equation; 3.3 Longitudinal static stability; 3.4 Lateral static stability; 3.5 Directional static stability; 3.6 Calculation of aircraft trim condition; References; Problems; Chapter 4. The equations of motion; 4.1 The equations of motion of a rigid symmetric aircraft; 4.2 The linearised equations of motion; 4.3 The decoupled equations of motion; 4.4 Alternative forms of the equations of motion; References; Problems; Chapter 5. The solution of the equations of motion 5.1 Methods of solution5.2 Cramer's rule; 5.3 Aircraft response transfer functions; 5.4 Response to controls; 5.5 Acceleration response transfer functions; 5.6 The state space method; 5.7 State space model augmentation; References; Problems; Chapter 6. Longitudinal dynamics; 6.1 Response to controls; 6.2 The dynamic stability modes; 6.3 Reduced order models; 6.4 Frequency response; 6.5 Flying and handling qualities; 6.6 Mode excitation; References; Problems; Chapter 7. Lateral-directional dynamics; 7.1 Response to controls; 7.2 The dynamic stability modes; 7.3 Reduced order models 7.4 Frequency response7.5 Flying and handling qualities; 7.6 Mode excitation; References; Problems; Chapter 8. Manoeuvrability; 8.1 Introduction; 8.2 The steady pull-up manoeuvre; 8.3 The pitching moment equation; 8.4 Longitudinal manoeuvre stability; 8.5 Aircraft dynamics and manoeuvrability; References; Chapter 9. Stability; 9.1 Introduction; 9.2 The characteristic equation; 9.3 The Routh-Hurwitz stability criterion; 9.4 The stability quartic; 9.5 Graphical interpretation of stability; References; Problems; Chapter 10. Flying and handling qualities; 10.1 Introduction 10.2 Short term dynamic models10.3 Flying qualities requirements; 10.4 Aircraft role; 10.5 Pilot opinion rating; 10.6 Longitudinal flying qualities requirements; 10.7 Control anticipation parameter; 10.8 Lateral-directional flying qualities requirements; 10.9 Flying qualities requirements on the s-plane; References; Problems; Chapter 11. Stability augmentation; 11.1 Introduction; 11.2 Augmentation system design; 11.3 Closed loop system analysis; 11.4 The root locus plot; 11.5 Longitudinal stability augmentation; 11.6 Lateral-directional stability augmentation; 11.7 The pole placement method References |
| Record Nr. | UNINA-9910457685103321 |
|
Cook M. V
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| Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Flight dynamics principles [[electronic resource] ] : [a linear systems approach to aircraft stability and control] / / M.V. Cook
| Flight dynamics principles [[electronic resource] ] : [a linear systems approach to aircraft stability and control] / / M.V. Cook |
| Autore | Cook M. V |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 |
| Descrizione fisica | 1 online resource (491 p.) |
| Disciplina |
629.1
629.1323 |
| Collana | Elsevier aerospace engineering series |
| Soggetto topico |
Aerodynamics
Flight Stability of airplanes |
| ISBN |
1-281-02927-0
9786611029272 0-08-055036-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front cover; Flight Dynamics Principles; Copyright page; Contents; Preface to the first edition; Preface to the second edition; Acknowledgements; Nomenclature; Chapter 1. Introduction; 1.1 Overview; 1.2 Flying and handling qualities; 1.3 General considerations; 1.4 Aircraft equations of motion; 1.5 Aerodynamics; 1.6 Computers; 1.7 Summary; References; Chapter 2. Systems of axes and notation; 2.1 Earth axes; 2.2 Aircraft body fixed axes; 2.3 Euler angles and aircraft attitude; 2.4 Axes transformations; 2.5 Aircraft reference geometry; 2.6 Controls notation; 2.7 Aerodynamic reference centres
ReferencesProblems; Chapter 3. Static equilibrium and trim; 3.1 Trim equilibrium; 3.2 The pitching moment equation; 3.3 Longitudinal static stability; 3.4 Lateral static stability; 3.5 Directional static stability; 3.6 Calculation of aircraft trim condition; References; Problems; Chapter 4. The equations of motion; 4.1 The equations of motion of a rigid symmetric aircraft; 4.2 The linearised equations of motion; 4.3 The decoupled equations of motion; 4.4 Alternative forms of the equations of motion; References; Problems; Chapter 5. The solution of the equations of motion 5.1 Methods of solution5.2 Cramer's rule; 5.3 Aircraft response transfer functions; 5.4 Response to controls; 5.5 Acceleration response transfer functions; 5.6 The state space method; 5.7 State space model augmentation; References; Problems; Chapter 6. Longitudinal dynamics; 6.1 Response to controls; 6.2 The dynamic stability modes; 6.3 Reduced order models; 6.4 Frequency response; 6.5 Flying and handling qualities; 6.6 Mode excitation; References; Problems; Chapter 7. Lateral-directional dynamics; 7.1 Response to controls; 7.2 The dynamic stability modes; 7.3 Reduced order models 7.4 Frequency response7.5 Flying and handling qualities; 7.6 Mode excitation; References; Problems; Chapter 8. Manoeuvrability; 8.1 Introduction; 8.2 The steady pull-up manoeuvre; 8.3 The pitching moment equation; 8.4 Longitudinal manoeuvre stability; 8.5 Aircraft dynamics and manoeuvrability; References; Chapter 9. Stability; 9.1 Introduction; 9.2 The characteristic equation; 9.3 The Routh-Hurwitz stability criterion; 9.4 The stability quartic; 9.5 Graphical interpretation of stability; References; Problems; Chapter 10. Flying and handling qualities; 10.1 Introduction 10.2 Short term dynamic models10.3 Flying qualities requirements; 10.4 Aircraft role; 10.5 Pilot opinion rating; 10.6 Longitudinal flying qualities requirements; 10.7 Control anticipation parameter; 10.8 Lateral-directional flying qualities requirements; 10.9 Flying qualities requirements on the s-plane; References; Problems; Chapter 11. Stability augmentation; 11.1 Introduction; 11.2 Augmentation system design; 11.3 Closed loop system analysis; 11.4 The root locus plot; 11.5 Longitudinal stability augmentation; 11.6 Lateral-directional stability augmentation; 11.7 The pole placement method References |
| Record Nr. | UNINA-9910784357203321 |
|
Cook M. V
|
||
| Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Flight dynamics principles [[electronic resource] ] : [a linear systems approach to aircraft stability and control] / / M.V. Cook
| Flight dynamics principles [[electronic resource] ] : [a linear systems approach to aircraft stability and control] / / M.V. Cook |
| Autore | Cook M. V |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 |
| Descrizione fisica | 1 online resource (491 p.) |
| Disciplina |
629.1
629.1323 |
| Collana | Elsevier aerospace engineering series |
| Soggetto topico |
Aerodynamics
Flight Stability of airplanes |
| ISBN |
1-281-02927-0
9786611029272 0-08-055036-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front cover; Flight Dynamics Principles; Copyright page; Contents; Preface to the first edition; Preface to the second edition; Acknowledgements; Nomenclature; Chapter 1. Introduction; 1.1 Overview; 1.2 Flying and handling qualities; 1.3 General considerations; 1.4 Aircraft equations of motion; 1.5 Aerodynamics; 1.6 Computers; 1.7 Summary; References; Chapter 2. Systems of axes and notation; 2.1 Earth axes; 2.2 Aircraft body fixed axes; 2.3 Euler angles and aircraft attitude; 2.4 Axes transformations; 2.5 Aircraft reference geometry; 2.6 Controls notation; 2.7 Aerodynamic reference centres
ReferencesProblems; Chapter 3. Static equilibrium and trim; 3.1 Trim equilibrium; 3.2 The pitching moment equation; 3.3 Longitudinal static stability; 3.4 Lateral static stability; 3.5 Directional static stability; 3.6 Calculation of aircraft trim condition; References; Problems; Chapter 4. The equations of motion; 4.1 The equations of motion of a rigid symmetric aircraft; 4.2 The linearised equations of motion; 4.3 The decoupled equations of motion; 4.4 Alternative forms of the equations of motion; References; Problems; Chapter 5. The solution of the equations of motion 5.1 Methods of solution5.2 Cramer's rule; 5.3 Aircraft response transfer functions; 5.4 Response to controls; 5.5 Acceleration response transfer functions; 5.6 The state space method; 5.7 State space model augmentation; References; Problems; Chapter 6. Longitudinal dynamics; 6.1 Response to controls; 6.2 The dynamic stability modes; 6.3 Reduced order models; 6.4 Frequency response; 6.5 Flying and handling qualities; 6.6 Mode excitation; References; Problems; Chapter 7. Lateral-directional dynamics; 7.1 Response to controls; 7.2 The dynamic stability modes; 7.3 Reduced order models 7.4 Frequency response7.5 Flying and handling qualities; 7.6 Mode excitation; References; Problems; Chapter 8. Manoeuvrability; 8.1 Introduction; 8.2 The steady pull-up manoeuvre; 8.3 The pitching moment equation; 8.4 Longitudinal manoeuvre stability; 8.5 Aircraft dynamics and manoeuvrability; References; Chapter 9. Stability; 9.1 Introduction; 9.2 The characteristic equation; 9.3 The Routh-Hurwitz stability criterion; 9.4 The stability quartic; 9.5 Graphical interpretation of stability; References; Problems; Chapter 10. Flying and handling qualities; 10.1 Introduction 10.2 Short term dynamic models10.3 Flying qualities requirements; 10.4 Aircraft role; 10.5 Pilot opinion rating; 10.6 Longitudinal flying qualities requirements; 10.7 Control anticipation parameter; 10.8 Lateral-directional flying qualities requirements; 10.9 Flying qualities requirements on the s-plane; References; Problems; Chapter 11. Stability augmentation; 11.1 Introduction; 11.2 Augmentation system design; 11.3 Closed loop system analysis; 11.4 The root locus plot; 11.5 Longitudinal stability augmentation; 11.6 Lateral-directional stability augmentation; 11.7 The pole placement method References |
| Record Nr. | UNINA-9910825103603321 |
|
Cook M. V
|
||
| Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
