Cover image for Performance, stability, dynamics, and control of airplanes
Title:
Performance, stability, dynamics, and control of airplanes
Personal Author:
Series:
AIAA education series
Edition:
2nd ed.
Publication Information:
Reston, VA : American Institute of Aeronautics and Astronautics, 2004
ISBN:
9781563475832

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30000010193139 TL671.4 P35 2004 Open Access Book Book
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30000010082729 TL671.4 P35 2004 Open Access Book Book
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Summary

Summary

This provides a comprehensive and integrated exposure to airplane performance, stability, dynamics, and flight control. Basic aerodynamics, dynamics, and linear control systems are presented. In this text, the airplane is assumed to be a rigid body, elastic deformations and their effects on airplane motion are not considered. Numerous solved examples illustrate theory and design methods. Several exercise problems with answers are included in each chapter to help the reader acquire problem-solving skills. In addition, Matlabae tools are used for the control design. In this second edition, several typographical errors are corrected, lists of symbols/nomenclature and tables of formulas are included to facilitate the reader.


Author Notes

Bandu N. Pamadi is a senior aerospace engineer at NASA Langley Research Center


Table of Contents

Prefacep. xv
Preface to the Previous Editionp. xvii
Chapter 1. Review of Basic Aerodynamic Principlesp. 1
1.1 Introductionp. 1
1.2 Fluid Flow over Wings and Bodiesp. 2
1.3 Drag of Bodiesp. 11
1.4 Wing Parametersp. 12
1.5 Aerodynamic Characteristics of Wing Sectionsp. 18
1.6 Aerodynamic Characteristics of Finite Wingsp. 27
1.7 Methods of Reducing Induced Dragp. 31
1.8 Tip Vortices: Formation and Hazardsp. 32
1.9 Flow of a Compressible Fluidp. 35
1.10 Aerodynamic Forces in Supersonic Flowp. 36
1.11 Critical Mach Numberp. 40
1.12 Area Rulep. 59
1.13 Summaryp. 64
Referencesp. 65
Problemsp. 66
Chapter 2. Aircraft Performancep. 67
2.1 Introductionp. 67
2.2 Equations of Motion for Flight in Vertical Planep. 70
2.3 Gliding Flightp. 73
2.4 Level Flightp. 81
2.5 Climbing Flightp. 94
2.6 Range and Endurancep. 106
2.7 Endurancep. 114
2.8 Turning Flightp. 122
2.9 Takeoff and Landingp. 146
2.10 Hazards During Takeoff and Landing: Windshear and Microburstp. 156
2.11 Summaryp. 158
Referencesp. 158
Problemsp. 159
Chapter 3. Static Stability and Controlp. 165
3.1 Introductionp. 165
3.2 Concept of Equilibrium and Stabilityp. 165
3.3 Static Longitudinal Stabilityp. 168
3.4 Stability in Maneuvering Flightsp. 249
3.5 Static Directional Stabilityp. 259
3.6 Lateral Stabilityp. 294
3.7 Summaryp. 313
Referencesp. 313
Problemsp. 314
Chapter 4. Equations of Motion and Estimation of Stability Derivativesp. 321
4.1 Introductionp. 321
4.2 Axes Systemsp. 322
4.3 Equations of Motion and Concept of Moving Axes Systemp. 361
4.4 Estimation of Stability Derivativesp. 391
4.5 Summaryp. 438
Referencesp. 439
Problemsp. 440
Chapter 5. Linear Systems, Theory, and Design: A Brief Reviewp. 443
5.1 Introductionp. 443
5.2 Laplace Transformp. 444
5.3 Transfer Functionp. 449
5.4 System Responsep. 450
5.5 Steady-State Errors of Unity Feedback Systemsp. 457
5.6 Frequency Responsep. 460
5.7 Stability of Closed-Loop Systemsp. 464
5.8 Relations Between Time-Domain and Frequency-Domain Parametersp. 488
5.9 Design of Compensatorsp. 491
5.10 State-Space Analysis and Designp. 510
5.11 Summaryp. 536
Referencesp. 536
Problemsp. 536
Chapter 6. Airplane Response and Closed-Loop Controlp. 541
6.1 Introductionp. 541
6.2 Longitudinal Responsep. 541
6.3 Lateral-Directional Responsep. 569
6.4 Flying Qualitiesp. 595
6.5 Closed-Loop Flight Controlp. 599
6.6 Summaryp. 626
Referencesp. 627
Problemsp. 627
Chapter 7. Inertia Coupling and Spinp. 631
7.1 Introductionp. 631
7.2 Inertia Couplingp. 631
7.3 Autorotation of Wings and Fuselagesp. 644
7.4 Airplane Spinp. 650
7.5 Equations of Motion for Steady-State Spinp. 653
7.6 Spin Recoveryp. 667
7.7 Geometrical Modifications to Improve Spin Resistancep. 668
7.8 Summaryp. 674
Referencesp. 675
Problemsp. 676
Chapter 8. Stability and Control Problems at High Angles of Attackp. 677
8.1 Introductionp. 677
8.2 A Brief Historical Sketchp. 677
8.3 Brief Overview of High-Alpha Problemsp. 678
8.4 Delta Wings at High Angles of Attackp. 680
8.5 Leading-Edge Extensionsp. 690
8.6 Forebodies at High Angles of Attackp. 694
8.7 Relation Between Angle of Attack, Sideslip, and Roll Anglep. 699
8.8 Wing Rockp. 699
8.9 Roll Attractor of Delta Wingsp. 714
8.10 Forebody-Induced Wing Rockp. 718
8.11 Suppression of Wing Rockp. 729
8.12 Roll Reversal and Yaw Departurep. 736
8.13 Control Concepts at High Angles of Attackp. 739
8.14 Summaryp. 753
Referencesp. 754
Appendix A. Standard Atmospheresp. 757
Appendix B. Table of Laplace Transformsp. 761
Appendix C. Cramer's Rulep. 763
Appendix D. Conversion of U.S. Customary Units to SI Unitsp. 765
Appendix E. Solved Examplesp. 767
Bibliographyp. 769
Indexp. 771
Series Listingp. 781