internetboekhandel.nl
buttons Home pagina Kassa pagina, Winkelwagentje Contact info Email ons
leeg Home pagina Kassa pagina, Winkelwagentje Contact info Email ons Home pagina Rijks
Boekenweek
Rijks Home pagina Home pagina Kassa pagina, Winkelwagentje Contact info Email ons Besteller 60
 
Nederlands Buitenlands   Alles  Titel  Auteur  ISBN        
Technische wetenschappen
Technische wetenschappen algemeen
Levertijd: 5 tot 11 werkdagen


Napolitano, Marcello

Aircraft Dynamics

€ 334.95

Napolitano`s Aircraft Dynamics is designed to help readers extrapolate from low level formulas, equations, and details to high level comprehensive views of the main concepts. the text also helps readers with fundamental skills of learning the "basic modeling" of the aircraft aerodynamics and dynamics.


Taal / Language : English

Inhoudsopgave:
1. Aircraft Equations of Motion

1.1 Introduction

1.2 Reference Frames and Assumptions

1.3 Conservation of the Linear Momentum Equations (CLMEs)

1.4 Conservation of the Angular Momentum Equations (CAMEs)

1.5 Conservation of the Angular Momentum Equations (CAMEs) with Rotor Effects

1.6 Euler Angles

1.7 Flight Path Equations (FPEs)

1.8 Kinematic Equations (KEs)

1.9 Gravity Equations (GEs)

1.10 Summary of the Aircraft Equations of Motion

1.11 Definition of Steady-State and Perturbation Conditions

1.12 Aircraft Equations of Motion at Steady-State Conditions

1.13 Aircraft Equations of Motion at Perturbed Conditions

1.14 Small Perturbation Equations from a Steady-State Level Flight

1.15 Summary

References

Student Sample Problems

Problems

2. Review of Basic Concepts of Aerodynamic Modeling

2.1 Introduction

2.2 Review of Key Aerodynamic Characteristics for Wing Sections

2.3 Wing Planforms and Wing Lift Curve Slope

2.4 Review of the Downwash Effect and Effectiveness of Control Surfaces

2.5 Determination of the Aerodynamic Center for Wing and Wing1Fuselage

2.6 Approaches to the Modeling of Aerodynamic Forces and Moments

2.7 Summary

References

Student Sample Problems

Problems

3. Modeling of Longitudinal Aerodynamic Forces and Moments

3.1 Introduction

3.2 Aircraft Stability Axes

3.3 Modeling of the Longitudinal Steady-State Aerodynamic Forces and Moment

3.4 Modeling of FAX1

3.5 Modeling of FAZ1

3.6 Modeling of MA1

3.7 Aircraft Aerodynamic Center

3.8 Summary of the Longitudinal Steady-State Aerodynamic Forces and Moment

3.9 Modeling of the Longitudinal Small Perturbation Aerodynamic Forces and Moments

3.10 Summary of Longitudinal Stability and Control Derivatives

3.11 Summary

References

Student Sample Problems

Case Study

Short Problems

Problems

4. Modeling of Lateral Directional Aerodynamic Forces and Moments

4.1 Introduction

4.2 Modeling of FAY1

4.3 Modeling of LA1

4.4 Modeling of NA1

4.5 Summary of the Lateral Directional Steady-State Force and Moments

4.6 Modeling of the Small Perturbation Lateral Directional Aerodynamic Force and Moments

4.7 Summary of Longitudinal and Lateral Directional Aerodynamic Stability and Control Derivatives

4.8 Final Overview and Ranking of the Importance of the Aerodynamic Coefficients

4.9 Summary of the Modeling of the Longitudinal and Lateral-Directional Aerodynamic Forces and Moments

References

Student Sample Problems

Case Study

Short Problems

Problems

5. Review of Basic Aircraft Performance and Modeling of Thrust Forces and Moments

5.1 Introduction

5.2 Review of Different Aircraft Propulsion Systems

5.3 Review of Basic Aircraft Performance

5.4 Power at Level Flight

5.5 Determination of Power Required

5.6 Determination of Power Available

5.7 Modeling of the Thrust Forces and Moments

5.8 Summary

References

Student Sample Problems

Problems

6. Aircraft Stability and Design for Trim Conditions

6.1 Introduction

6.2 Concept of Aircraft Stability

6.3 Criteria for Aircraft Static Stability

6.4 Longitudinal Analysis of Steady-State Straight Flight

6.5 Lift Chart and Trim Diagram

6.6 Lateral Directional Analysis of Steady-State Straight Flight

6.7 Summary

References

Student Sample Problems

Problems

7. Solution of the Aircraft Equations of Motion Based on Laplace Transformations and Transfer Functions

7.1 Introduction

7.2 Application of Laplace Transformations to the Longitudinal Small Perturbation Equations

7.3 Routh-Hurwitz Analysis of the Longitudinal Stability

7.4 Longitudinal Dynamic Modes: Short Period and Phugoid

7.5 Solution of the Longitudinal Equations

7.6 Short Period Approximation

7.7 Phugoid Approximation

7.8 Summary of the Longitudinal Equations

7.9 Application of Laplace Transformations to the Lateral Directional Small Perturbation Equations

7.10 Routh-Hurwitz Analysis of the Lateral Directional Stability

7.11 Lateral Directional Dynamic Modes: Rolling, Spiral, and Dutch Roll

7.12 Solution of the Lateral Directional Equations

7.13 Rolling Approximation

7.14 Summary of Lateral Directional Equations

7.15 Sensitivity Analysis for the Aircraft Dynamics

7.16 Summary

References

Student Sample Problems

Problems

8. State Variable Modeling of the Aircraft Dynamics

8.1 Introduction

8.2 Introduction to State Variables for Nonlinear Systems

8.3 Introduction to State Variables for Linear/Literalized Systems

8.4 State Variable Modeling of the Longitudinal Dynamics

8.5 State Variable Modeling of the Lateral Directional Dynamics

8.6 Augmentation of the Aircraft State Variable Modeling

8.7 Summary of State Variable Modeling of the Aircraft Dynamics

8.8 Summary

References

Student Sample Problems

Problems

9. Introduction to Modern Flight Simulation Codes

9.1 Introduction

9.2 Introduction to the Flight Dynamics & Control (FDC) Toolbox

9.3 Introduction to the Aerospace Blockset by Mathworks

9.4 Introduction to AIRLIB

9.5 Summary

References

Student Sample Problems

10. Pilot Ratings and Aircraft Handling Qualities

10.1 Introduction

10.2 Aircraft Flight Envelope

10.3 Levels of Aircraft Flying Qualities: Cooper-Harper Pilot Rating

10.4 Classes of Aircraft

10.5 Classification of Aircraft Maneuvers and Mission Profile

10.6 Flying Quality Requirements for the Longitudinal Dynamics

10.7 Flying Quality Requirements for the Lateral Directional Dynamics

10.8 Summary

References

Appendix A Review of Useful Topics

Appendix B Data for Different Aircraft

Appendix C Detailed Drawings for Different Aircraft
Extra informatie: 
Hardback
720 pagina's
Januari 2011
1496 gram
277 x 222 x 29 mm
John Wiley & Sons us

Levertijd: 5 tot 11 werkdagen