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Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops / / Zachary T. Applin and Paul L. Coe, Jr
| Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops / / Zachary T. Applin and Paul L. Coe, Jr |
| Autore | Applin Zachary T. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 |
| Descrizione fisica | 1 online resource (iii, 63 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Aerodynamic stability
Aerodynamic characteristics Transport aircraft Propellers Control stability Turboprop transports Stability of airplanes |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709793703321 |
Applin Zachary T.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Mass distribution and performance of free flight models / / by Max Scherberg and R.V. Rhode
| Mass distribution and performance of free flight models / / by Max Scherberg and R.V. Rhode |
| Autore | Scherberg Max G. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1927 |
| Descrizione fisica | 1 online resource (25 pages, 3 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Stability of airplanes
Airplanes - Weight Airplanes - Models - Testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713673603321 |
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Scherberg Max G.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1927 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A mechanical device for illustrating airplane stability / / by F.E. Norton
| A mechanical device for illustrating airplane stability / / by F.E. Norton |
| Autore | Norton F. H (Frederick Harwood), <1896-1992, > |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1921 |
| Descrizione fisica | 1 online resource (5 pages, 1 unnumbered page) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Stability of airplanes
Measuring instruments |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713070503321 |
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Norton F. H (Frederick Harwood), <1896-1992, >
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| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1921 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Motion of the two-control airplane in rectilinear flight after initial disturbances with introduction of controls following an exponential law / / by Alexander Klemin
| Motion of the two-control airplane in rectilinear flight after initial disturbances with introduction of controls following an exponential law / / by Alexander Klemin |
| Autore | Klemin Alexander <1888-1950, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 |
| Descrizione fisica | 1 online resource (30 pages, 10 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Stability of airplanes
Airplanes - Control Equations of motion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716726903321 |
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Klemin Alexander <1888-1950, >
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Performance, stability, dynamics, and control of airplanes [[electronic resource] /] / Bandu N. Pamadi
| Performance, stability, dynamics, and control of airplanes [[electronic resource] /] / Bandu N. Pamadi |
| Autore | Pamadi Bandu N. <1945-> |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2004 |
| Descrizione fisica | xix, 780 p. : ill |
| Disciplina | 629.13 |
| Collana | AIAA education series |
| Soggetto topico |
Airplanes - Performance
Stability of airplanes Airplanes - Control systems Aerodynamics |
| Soggetto genere / forma | Electronic books. |
| ISBN | 1-60086-099-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910454405503321 |
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Pamadi Bandu N. <1945->
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| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2004 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Performance, stability, dynamics, and control of airplanes [[electronic resource] /] / Bandu N. Pamadi
| Performance, stability, dynamics, and control of airplanes [[electronic resource] /] / Bandu N. Pamadi |
| Autore | Pamadi Bandu N. <1945-> |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2004 |
| Descrizione fisica | xix, 780 p. : ill |
| Disciplina | 629.13 |
| Collana | AIAA education series |
| Soggetto topico |
Airplanes - Performance
Stability of airplanes Airplanes - Control systems Aerodynamics |
| ISBN | 1-60086-099-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910782755203321 |
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Pamadi Bandu N. <1945->
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| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2004 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Performance, stability, dynamics, and control of airplanes [[electronic resource] /] / Bandu N. Pamadi
| Performance, stability, dynamics, and control of airplanes [[electronic resource] /] / Bandu N. Pamadi |
| Autore | Pamadi Bandu N. <1945-> |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2004 |
| Descrizione fisica | xix, 780 p. : ill |
| Disciplina | 629.13 |
| Collana | AIAA education series |
| Soggetto topico |
Airplanes - Performance
Stability of airplanes Airplanes - Control systems Aerodynamics |
| ISBN | 1-60086-099-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910811086303321 |
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Pamadi Bandu N. <1945->
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| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2004 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Preliminary stability and control tests in the NACA free-flight wind tunnel and correlation with full-scale flight tests / / by Joseph A. Shortal and Clatyon J. Osterhout
| Preliminary stability and control tests in the NACA free-flight wind tunnel and correlation with full-scale flight tests / / by Joseph A. Shortal and Clatyon J. Osterhout |
| Autore | Shortal Joseph Adams <1908-> |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 |
| Descrizione fisica | 1 online resource (19 pages, 10 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Control
Stability of airplanes Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717251403321 |
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Shortal Joseph Adams <1908->
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Span load distribution on two monoplane wing models as affected by twist and sweepback / / by Montgomery Knight and Richard W. Noyes
| Span load distribution on two monoplane wing models as affected by twist and sweepback / / by Montgomery Knight and Richard W. Noyes |
| Autore | Knight Montgomery |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930 |
| Descrizione fisica | 1 online resource (7 pages, 12 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Loads (Mechanics) Stability of airplanes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714048703321 |
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Knight Montgomery
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Stability and control of aircraft systems [[electronic resource] ] : introduction to classical feedback control / / Roy Langton
| Stability and control of aircraft systems [[electronic resource] ] : introduction to classical feedback control / / Roy Langton |
| Autore | Langton Roy |
| Pubbl/distr/stampa | Chichester, England ; ; Hoboken, NJ, : Wiley, c2006 |
| Descrizione fisica | 1 online resource (256 p.) |
| Disciplina |
629.13236
629.83 |
| Collana | Aerospace series |
| Soggetto topico |
Stability of airplanes
Airplanes - Control |
| Soggetto genere / forma | Electronic books. |
| ISBN |
0-470-05848-X
1-280-72117-0 9786610721177 0-470-05849-8 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Stability and Control of AircraftSystems; Contents; Series Preface; Preface; 1 Developing the Foundation; 1.1 Engineering Units; 1.1.1 International System of Units (SI); 1.1.2 US/Imperial Units System; 1.1.3 Comparing the SI and US/Imperial Units Systems; 1.2 Block Diagrams; 1.2.1 Examples of Summation (or Comparison) Devices; 1.3 Differential Equations; 1.3.1 Using the 'D' Notation; 1.4 Spring-Mass System Example; 1.4.1 The Standard Form of Second-order System Transfer Function; 1.5 Primer on Complex Numbers; 1.5.1 The Complex Sinusoid; 1.6 Chapter Summary; 2 Closing the Loop
2.1 The Generic Closed Loop System2.1.1 The Simplest Form of Closed Loop System; 2.2 The Concept of Stability; 2.3 Response Testing of Control Systems; 2.4 The Integration Process; 2.5 Hydraulic Servo-actuator Example; 2.6 Calculating Frequency Response; 2.6.1 Frequency Response of a First-order Lag; 2.6.2 Frequency Response of a Second-order System; 2.7 Aircraft Flight Control System Example; 2.7.1 Control System Assumptions; 2.7.2 Open Loop Analysis; 2.7.3 Closed Loop Performance; 2.8 Alternative Graphical Methods for Response Analysis; 2.8.1 The Nyquist Diagram 2.8.2 Deriving Closed Loop Response from Nyquist Diagrams2.8.3 The Nichols Chart; 2.8.4 Graphical Methods - Summary Comments and Suggestions; 2.9 Chapter Summary; 3 Control System Compensation Techniques; 3.1 Control System Requirements; 3.2 Compensation Methods; 3.2.1 Proportional Plus Integral Control; 3.2.2 Proportional Plus Integral Plus Derivative Control; 3.2.3 Lead-Lag Compensation; 3.2.4 Lag-Lead Compensation; 3.2.5 Feedback Compensation; 3.3 Applications of Control Compensation; 3.3.1 Proportional Plus Integral Example; 3.3.2 Lead-Lag Compensation Example 3.3.3 Class 2 System Design Example3.4 Chapter Summary; 4 Introduction to Laplace Transforms; 4.1 An Overview of the Application of Laplace Transforms; 4.2 The Evolution of the Laplace Transform; 4.2.1 Proof of the General Case; 4.3 Applying Laplace Transforms to Linear Systems Analysis; 4.3.1 Partial Fractions; 4.4 Laplace Transforms - Summary of Key Points; 4.5 Root Locus; 4.5.1 Root Locus Construction Rules; 4.5.2 Connecting Root Locus to Conventional Linear Analysis; 4.6 Root Locus Example; 4.7 Chapter Summary; 5 Dealing with Nonlinearities; 5.1 Definition of Nonlinearity Types 5.2 Continuous Nonlinearities5.2.1 Engine Fuel Control System Example; 5.3 Discontinuous Nonlinearities; 5.3.1 Stability Analysis with Discontinuous Nonlinearities; 5.4 The Transport Delay; 5.5 Simulation; 5.6 Chapter Summary; 6 Electronic Controls; 6.1 Analog Electronic Controls; 6.1.1 The Operational Amplifier; 6.1.2 Building Analog Control Algorithms; 6.2 The Digital Computer as a Dynamic Control Element; 6.2.1 Signal Conversion; 6.2.2 Digital Controller Architectures; 6.3 The Stability Impact of Digital Controls; 6.4 Digital Control Design Example; 6.5 Creating Digital Control Algorithms 6.5.1 The Integrator |
| Record Nr. | UNINA-9910143736303321 |
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Langton Roy
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| Chichester, England ; ; Hoboken, NJ, : Wiley, c2006 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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