Muutke küpsiste eelistusi

Aircraft Dynamics: From Modeling to Simulation [Kõva köide]

4.17/5 (24 hinnangut Goodreads-ist)
(West Virginia University)
  • Formaat: Hardback, 720 pages, kõrgus x laius x paksus: 285x213x33 mm, kaal: 1746 g
  • Ilmumisaeg: 20-Dec-2011
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 0470626674
  • ISBN-13: 9780470626672
Teised raamatud teemal:
Aircraft Dynamics: From Modeling to SimulationSuurem pilt
  • Formaat: Hardback, 720 pages, kõrgus x laius x paksus: 285x213x33 mm, kaal: 1746 g
  • Ilmumisaeg: 20-Dec-2011
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 0470626674
  • ISBN-13: 9780470626672
Teised raamatud teemal:
Püsilink: https://www.kriso.ee/db/9780470626672.html
Märksõnad:
The 1st edition of Aircraft Dynamics: from Modeling to Simulation by Marcello R. Napolitano is an innovative textbook with specific features for assisting, motivating and engaging aeronautical/aerospace engineering students in the challenging task of understanding the basic principles of aircraft dynamics and the necessary skills for the modeling of the aerodynamic and thrust forces and moments.  Additionally the textbook provides a detailed introduction to the development of simple but very effective simulation environments for today demanding students as well as professionals.  The book contains an abundance of real life students sample problems and problems along with very useful Matlab® codes.
1 Aircraft Equations of Motion 1(36)
1.1 Introduction
1(1)
1.2 Reference Frames and Assumptions
2(1)
1.3 Conservation of the Linear Momentum Equations (CLMEs)
3(3)
1.4 Conservation of the Angular Momentum Equations (CAMEs)
6(4)
1.5 Conservation of the Angular Momentum Equations (CAMEs) with Rotor Effects
10(1)
1.6 Euler Angles
11(1)
1.7 Flight Path Equations (FPEs)
12(2)
1.8 Kinematic Equations (KEs)
14(2)
1.9 Gravity Equations (GEs)
16(1)
1.10 Summary of the Aircraft Equations of Motion
16(1)
1.11 Definition of Steady-State and Perturbation Conditions
17(1)
1.12 Aircraft Equations of Motion at Steady-State Conditions
18(1)
1.13 Aircraft Equations of Motion at Perturbed Conditions
19(3)
1.14 Small Perturbation Equations from a Steady-State Level Flight
22(1)
1.15 Summary
23(3)
References
26(1)
Student Sample Problems
26(6)
Problems
32(5)
2 Review of Basic Concepts of Aerodynamic Modeling 37(41)
2.1 Introduction
37(1)
2.2 Review of Key Aerodynamic Characteristics for Wing Sections
37(5)
2.3 Wing Planforms and Wing Lift Curve Slope
42(6)
2.4 Review of the Downwash Effect and Effectiveness of Control Surfaces
48(5)
2.5 Determination of the Aerodynamic Center for Wing and Wing + Fuselage
53(4)
2.6 Approaches to the Modeling of Aerodynamic Forces and Moments
57(3)
2.6.1 Wind Tunnel Analysis
57(1)
2.6.2 CFD Analysis
58(1)
2.6.3 Parameter IDentification from Flight Data
59(1)
2.6.4 Correlation from Wind Tunnel Data and Empirical "Build-Up" Analysis
60(1)
2.7 Summary
60(1)
References
61(1)
Student Sample Problems
62(13)
Problems
75(3)
3 Modeling of Longitudinal Aerodynamic Forces and Moments 78(57)
3.1 Introduction
78(1)
3.2 Aircraft Stability Axes
79(1)
3.3 Modeling of the Longitudinal Steady-State Aerodynamic Forces and Moment
79(1)
3.4 Modeling of FAX1
80(3)
3.5 Modeling of FAZ1
83(4)
3.6 Modeling of MA1
87(2)
3.7 Aircraft Aerodynamic Center
89(2)
3.8 Summary of the Longitudinal Steady-State Aerodynamic Forces and Moment
91(1)
3.9 Modeling of the Longitudinal Small Perturbation Aerodynamic Forces and Moments
91(5)
3.9.1 Modeling of (cD1, cL1, cm1)
93(1)
3.9.2 Modeling of (cDu, cLu, cmu)
93(1)
3.9.3 Modeling of (cDα, cLα, cmα) and (cDq, cLq, cmq)
94(2)
3.10 Summary of Longitudinal Stability and Control Derivatives
96(4)
3.11 Summary
100(1)
References
100(1)
Student Sample Problems
101(9)
Case Study
110(17)
Short Problems
127(1)
Problems
128(7)
4 Modeling of Lateral Directional Aerodynamic Forces and Moments 135(133)
4.1 Introduction
135(2)
4.2 Modeling of FAY1
137(12)
4.2.1 Conceptual Modeling of CYβ
138(2)
4.2.2 Mathematical Modeling of CYβ
140(7)
4.2.3 Modeling of CYδA
147(1)
4.2.4 Modeling of CYδR
147(2)
4.3 Modeling of LA1
149(19)
4.3.1 Conceptual Modeling of clβ
150(5)
4.3.2 Mathematical Modeling of clβ
155(5)
4.3.3 Modeling of clδA
160(6)
4.3.4 Modeling of clδR
166(2)
4.4 Modeling of NA1
168(9)
4.4.1 Conceptual Modeling of cnβ
169(3)
4.4.2 Mathematical Modeling of cnβ
172(2)
4.4.3 Modeling of cnδA
174(2)
4.4.4 Modeling of cnδR
176(1)
4.5 Summary of the Lateral Directional Steady-State Force and Moments
177(1)
4.6 Modeling of the Small Perturbation Lateral Directional Aerodynamic Force and Moments
178(11)
4.6.1 Modeling of cYβ, clβ, cnβ
180(1)
4.6.2 Modeling of cYp
180(1)
4.6.3 Modeling of clp
181(2)
4.6.4 Modeling of cnp
183(2)
4.6.5 Modeling of cYr
185(1)
4.6.6 Modeling of clr
185(2)
4.6.7 Modeling of cnr
187(2)
4.7 Summary of Longitudinal and Lateral Directional Aerodynamic Stability and Control Derivatives
189(7)
4.8 Final Overview and Ranking of the Importance of the Aerodynamic Coefficients
196(2)
4.9 Summary of the Modeling of the Longitudinal and Lateral-Directional Aerodynamic Forces and Moments
198(2)
References
200(1)
Student Sample Problems
200(36)
Case Study
236(26)
Short Problems
262(1)
Problems
263(5)
5 Review of Basic Aircraft Performance and Modeling of Thrust Forces and Moments 268(37)
5.1 Introduction
268(1)
5.2 Review of Different Aircraft Propulsion Systems
268(5)
5.2.1 Piston Engine (Propeller) Aircraft Engines
269(1)
5.2.2 Turboprop Aircraft Engines
270(1)
5.2.3 Turbojet Aircraft Engines
271(1)
5.2.4 Turbofan Aircraft Engines
272(1)
5.2.5 Ramjet Aircraft Engines
273(1)
5.3 Review of Basic Aircraft Performance
273(1)
5.4 Power at Level Flight
274(5)
5.4.1 Maximum Aerodynamic Efficiency
275(1)
5.4.2 Minimum Aerodynamic Drag
275(2)
5.4.3 Minimum Power Required
277(2)
5.5 Determination of Power Required
279(3)
5.6 Determination of Power Available
282(5)
5.7 Modeling of the Thrust Forces and Moments
287(7)
5.7.1 Modeling of the Steady-State Thrust Forces and Moments
288(3)
5.7.2 Modeling of the Small Perturbation Thrust Forces and Moments
291(3)
5.8 Summary
294(2)
References
296(1)
Student Sample Problems
296(8)
Problems
304(1)
6 Aircraft Stability and Design for Trim Conditions 305(47)
6.1 Introduction
305(1)
6.2 Concept of Aircraft Stability
305(1)
6.3 Criteria for Aircraft Static Stability
306(7)
6.3.1 Static Stability Criteria #1 (SSC #1)
307(1)
6.3.2 Static Stability Criteria #2 (SSC #2)
308(1)
6.3.3 Static Stability Criteria #3 (SSC #3)
308(1)
6.3.4 Static Stability Criteria #4 (SSC #4)
309(1)
6.3.5 Static Stability Criteria #5 (SSC #5)
310(1)
6.3.6 Static Stability Criteria #5, #6, and #7 (SSC #5, SSC #6, SSC #7)
311(1)
6.3.7 Static Stability Criteria #9 (SSC #9)
311(1)
6.3.8 Static Stability Criteria #10 (SSC #10)
312(1)
6.4 Longitudinal Analysis of Steady-State Straight Flight
313(9)
6.5 Lift Chart and Trim Diagram
322(10)
6.5.1 Lift Chart
322(2)
6.5.2 Trim Diagram
324(5)
6.5.3 Trim Diagrams for Different Classes of Aircraft
329(1)
6.5.4 Trim Diagrams for Thrust Axis Above/Below Center of Gravity
329(3)
6.6 Lateral Directional Analysis of Steady-State Straight Flight
332(8)
6.7 Summary
340(1)
References
340(1)
Student Sample Problems
340(9)
Problems
349(3)
7 Solution of the Aircraft Equations of Motion Based on Laplace Transformations and Transfer Functions 352(80)
7.1 Introduction
352(1)
7.2 Application of Laplace Transformations to the Longitudinal Small Perturbation Equations
353(5)
7.3 Routh-Hurwitz Analysis of the Longitudinal Stability
358(2)
7.4 Longitudinal Dynamic Modes: Short Period and Phugoid
360(1)
7.5 Solution of the Longitudinal Equations
361(2)
7.6 Short Period Approximation
363(3)
7.7 Phugoid Approximation
366(3)
7.8 Summary of the Longitudinal Equations
369(2)
7.9 Application of Laplace Transformations to the Lateral Directional Small Perturbation Equations
371(5)
7.10 Routh-Hurwitz Analysis of the Lateral Directional Stability
376(1)
7.11 Lateral Directional Dynamic Modes: Rolling, Spiral, and Dutch Roll
377(2)
7.12 Solution of the Lateral Directional Equations
379(3)
7.13 Rolling Approximation
382(3)
7.14 Summary of Lateral Directional Equations
385(1)
7.15 Sensitivity Analysis for the Aircraft Dynamics
386(21)
7.15.1 Short Period Sensitivity Analysis
387(7)
7.15.2 Phugoid Sensitivity Analysis
394(4)
7.15.3 Sensitivity Analysis for the Lateral Directional Parameters
398(9)
7.16 Summary
407(1)
References
407(1)
Student Sample Problems
407(23)
Problems
430(2)
8 State Variable Modeling of the Aircraft Dynamics 432(44)
8.1 Introduction
432(1)
8.2 Introduction to State Variables for Nonlinear Systems
433(1)
8.3 Introduction to State Variables for Linear/Linearized Systems
433(2)
8.4 State Variable Modeling of the Longitudinal Dynamics
435(5)
8.5 State Variable Modeling of the Lateral Directional Dynamics
440(5)
8.6 Augmentation of the Aircraft State Variable Modeling
445(2)
8.6.1 Modeling of the Altitude (h)
445(1)
8.6.2 Modeling of the Flight Path Angle (γ)
446(1)
8.6.3 Modeling of the Engine Dynamics
446(1)
8.6.4 Modeling of the Actuator Dynamics
446(1)
8.6.5 Modeling of the Atmospheric Turbulence
447(1)
8.7 Summary of State Variable Modeling of the Aircraft Dynamics
447(3)
8.8 Summary
450(1)
References
450(1)
Student Sample Problems
450(20)
Problems
470(6)
9 Introduction to Modern Flight Simulation Codes 476(47)
9.1 Introduction
476(3)
9.2 Introduction to the Flight Dynamics & Control (FDC) Toolbox
479(24)
9.2.1 Equations of Motion within the FDC Simulation Environment
479(4)
9.2.2 FDC Modeling of Beaver Aerodynamic Forces and Moments
483(2)
9.2.3 Alternative Approach for FDC Modeling of Aerodynamic Forces and Moments
485(1)
9.2.4 Case Study #1: FDC Modeling of Look-Up Tables Based Aerodynamic Coefficients
486(7)
9.2.5 FDC Modeling of the Gravity Force
493(1)
9.2.6 FDC Modeling of the Atmospheric Turbulence Force
493(1)
9.2.7 FDC Modeling of the Beaver Propulsive Forces and Moments
494(2)
9.2.8 Case Study #2: FDC Modeling of Propulsive Forces and Moments
496(2)
9.2.9 Auxiliary FDC Blocks
498(5)
9.2.10 Additional FDC Blocks
503(1)
9.3 Introduction to the Aerospace Blockset by Mathworks
503(9)
9.3.1 General Organization of the Aerospace Blockset
503(1)
9.3.2 Introduction to the Environment Library
504(2)
9.3.3 Introduction to the Flight Parameters Library
506(1)
9.3.4 Introduction to the Equations of Motion Library
506(2)
9.3.5 Introduction to the Aerodynamics Library
508(1)
9.3.6 Introduction to the Propulsion Library
508(1)
9.3.7 Introduction to the Utilities Library
509(1)
9.3.8 Introduction to the Mass Properties Library
510(1)
9.3.9 Introduction to the Actuators Library
511(1)
9.3.10 Introduction to the GNC and Animation Libraries
511(1)
9.4 Introduction to AIRLIB
512(6)
9.4.1 AIRLIB's Strucure
512(1)
9.4.2 Generic Aircraft Model: Continuous-time Block
512(3)
9.4.3 Generic Aircraft Model: Discrete-time Block
515(1)
9.4.4 Collection of Aircraft Models
516(1)
9.4.5 Alternative Model Implementation
517(1)
9.4.6 Additional Tools within AIRLIB: The Function 'air3m'
517(1)
9.4.7 Additional Tools within AIRLIB: The Function 'ab2dv'
518(1)
9.5 Summary
518(1)
References
518(1)
Student Sample Problems
519(4)
10 Pilot Ratings and Aircraft Handling Qualities 523(18)
10.1 Introduction
523(1)
10.2 Aircraft Flight Envelope
524(2)
10.3 Levels of Aircraft Flying Qualities: Cooper-Harper Pilot Rating
526(5)
10.3.1 Aircraft Control Authority
526(1)
10.3.2 Pilot Workload
526(3)
10.3.3 Pilot Compensation
529(1)
10.3.4 Levels of Flying Qualities
529(2)
10.4 Classes of Aircraft
531(1)
10.5 Classification of Aircraft Maneuvers and Mission Profile
531(1)
10.6 Flying Quality Requirements for the Longitudinal Dynamics
532(4)
10.6.1 Longitudinal Control Forces
533(2)
10.6.2 Requirements for the Damping for the Phugoid Mode
535(1)
10.6.3 Requirements for the Short Period Mode
536(1)
10.7 Flying Quality Requirements for the Lateral Directional Dynamics
536(5)
10.7.1 Lateral Directional Control Forces
536(2)
10.7.2 Requirements for the Dutch Roll Mode
538(1)
10.7.3 Requirements for the Spiral Mode
539(1)
10.7.4 Requirements for the Rolling Mode
539(1)
10.7.5 Requirements for the Roll Control Effectiveness
539(2)
10.7.6 Additional Requirements for Steady Sideslips
541(1)
10.8 Summary
541(1)
References 541(2)
Appendix A Review of Useful Topics 543(41)
Appendix A.1 Review of Vector Operations
544(4)
Appendix A.2 Review of Matrix Operations
548(10)
Appendix A.3 Review of Center of Gravity and Inertial Properties
558(6)
Appendix A.4 Review of Application of Laplace Transform to Linear Constant Coefficients Differential Equations
564(11)
Appendix A.5 Review of First and Second Order Systems
575(6)
Appendix A.6 Review of Standard Atmospheric Model
581(3)
Appendix B Data for Different Aircraft 584(32)
Appendix B.1 Introduction
584(2)
Appendix B.2 Aircraft 1 Cessna 182
586(3)
Appendix B.3 Aircraft 2 Cessna 310
589(3)
Appendix B.4 Aircraft 3 Beech 99
592(3)
Appendix B.5 Aircraft 4 Cessna T37-A
595(3)
Appendix B.6 Aircraft 5 Cessna 620
598(3)
Appendix B.7 Aircraft 6 Learjet 24
601(3)
Appendix B.8 Aircraft 7 Boeing 747-200
604(3)
Appendix B.9 Aircraft 8 SIAI Marchetti S-211
607(3)
Appendix B.10 Aircraft 9 Lockheed F-104
610(3)
Appendix B.11 Aircraft 10 McDonnell Douglas F-4
613(2)
Reference
615(1)
Appendix C Detailed Drawings for Different Aircraft 616(87)
Appendix C.1 Introduction
617(1)
Appendix C.2 Aircraft 1 Aeritalia Fiat G-91
618(3)
Appendix C.3 Aircraft 2 Beech 99
621(3)
Appendix C.4 Aircraft 3 Boeing B52
624(3)
Appendix C.5 Aircraft 4 Boeing B727-200
627(3)
Appendix C.6 Aircraft 5 Boeing B737-600
630(3)
Appendix C.7 Aircraft 6 Boeing B747-200
633(4)
Appendix C.8 Aircraft 7 Boeing B757-200
637(3)
Appendix C.9 Aircraft 8 Boeing B767-200
640(3)
Appendix C.10 Aircraft 9 Cessna Citation CJ3
643(2)
Appendix C.11 Aircraft 10 Cessna T37
645(4)
Appendix C.12 Aircraft 11 General Dynamics F-16
649(3)
Appendix C.13 Aircraft 12 Grumman F-14
652(3)
Appendix C.14 Aircraft 13 Learjet 24
655(3)
Appendix C.15 Aircraft 14 Lockheed F-104
658(3)
Appendix C.16 Aircraft 15 Lockheed F-22
661(3)
Appendix C.17 Aircraft 16 Lockheed L-1011
664(3)
Appendix C.18 Aircraft 17 McDonnell Douglas C-17
667(3)
Appendix C.19 Aircraft 18 McDonnell Douglas DC-8
670(3)
Appendix C.20 Aircraft 19.1 McDonnell Douglas DC-9 Series 10
673(4)
Appendix C.21 Aircraft 19.2 McDonnell Douglas DC-9 Series 30
677(2)
Appendix C.22 Aircraft 19.3 McDonnell Douglas DC-9 Series 40
679(2)
Appendix C.23 Aircraft 19.4 McDonnell Douglas DC-9 Series 50
681(2)
Appendix C.24 Aircraft 20 McDonnell Douglas DC-10
683(3)
Appendix C.25 Aircraft 21 McDonnell Douglas F-4
686(3)
Appendix C.26 Aircraft 22 McDonnell Douglas F-15
689(3)
Appendix C.27 Aircraft 23 Rockwell B-1
692(3)
Appendix C.28 Aircraft 24 SIAI Marchetti S211
695(4)
Appendix C.29 Aircraft 25 Supermarine Spitfire
699(4)
Index 703
Marcello Napolitano is a Professor of Mechanical and Aerospace Engineering at West Virgina University, and has received numerous teaching, research and professional awards, including 11 teaching awards, 4 research awards and the NASA Outstanding Service Achievement Award. He is recognized as an authority on the subject of?Aircraft Dynamics.