000			05377nam a22004933i 4500
001			EBC3111614
003			MiAaPQ
005			20240729124523.0
006			m o d |
007			cr cnu||||||||
008			240724s2000 xx o ||||0 eng d
020			_a9781600860997 _q(electronic bk.)
020			_z9781563475832
035			_a(MiAaPQ)EBC3111614
035			_a(Au-PeEL)EBL3111614
035			_a(CaPaEBR)ebr10516719
035			_a(OCoLC)922979020
040			_aMiAaPQ _beng _erda _epn _cMiAaPQ _dMiAaPQ
050		4	_aTL671.4 -- .P28 2004eb
082	0		_a629.13
100	1		_aPamadi, Bandu N.
245	1	0	_aPerformance, Stability, Dynamics, and Control of Airplanes.
250			_a2nd ed.
264		1	_aReston : _bAmerican Institute of Aeronautics and Astronautics, _c2000.
264		4	_c©2004.
300			_a1 online resource (800 pages)
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
490	1		_aAIAA Education Series
505	0		_aCover -- Title -- Copyright -- Table of Contents -- Preface -- Preface to the Previous Edition -- Chapter 1. Review of Basic Aerodynamic Principles -- 1.1 Introduction -- 1.2 Fluid Flow over Wings and Bodies -- 1.3 Drag of Bodies -- 1.4 Wing Parameters -- 1.5 Aerodynamic Characteristics of Wing Sections -- 1.6 Aerodynamic Characteristics of Finite Wings -- 1.7 Methods of Reducing Induced Drag -- 1.8 Tip Vortices: Formation and Hazards -- 1.9 Flow of a Compressible Fluid -- 1.10 Aerodynamic Forces in Supersonic Flow -- 1.11 Critical Mach Number -- 1.12 Area Rule -- Summary -- References -- Problems -- Chapter 2. Aircraft Performance -- 2.1 Introduction -- 2.2 Equations of Motion for Flight in Vertical Plane -- 2.3 Gliding Flight -- 2.4 Level Flight -- 2.5 Climbing Flight -- 2.6 Range and Endurance -- 2.7 Endurance -- 2.8 Turning Flight -- 2.9 Takeoff and Landing -- 2.10 Hazards During Takeoff and Landing: Windshear and Microburst -- Summary -- References -- Problems -- Chapter 3. Static Stability and Control -- 3.1 Introduction -- 3.2 Concept of Equilibrium and Stability -- 3.3 Static Longitudinal Stability -- 3.4 Stability in Maneuvering Flights -- 3.5 Static Directional Stability -- 3.6 Lateral Stability -- 3.7 Summary -- References -- Problems -- Chapter 4. Equations of Motion and Estimation of Stability Derivatives -- 4.1 Introduction -- 4.2 Axes Systems -- 4.3 Equations of Motion and Concept of Moving Axes System -- 4.4 Estimation of Stability Derivatives -- 4.5 Summary -- References -- Problems -- Chapter 5. Linear Systems, Theory, and Design: A Brief Review -- 5.1 Introduction -- 5.2 Laplace Transform -- 5.3 Transfer Function -- 5.4 System Response -- 5.5 Steady-State Errors of Unity Feedback Systems -- 5.6 Frequency Response -- 5.7 Stability of Closed-Loop Systems -- 5.8 Relations Between Time-Domain and Frequency-Domain Parameters.
505	8		_a5.9 Design of Compensators -- 5.10 State-Space Analysis and Design -- 5.11 Summary -- References -- Problems -- Chapter 6. Airplane Response and Closed-Loop Control -- 6.1 Introduction -- 6.2 Longitudinal Response -- 6.3 Lateral-Directional Response -- 6.4 Flying Qualities -- 6.5 Closed-Loop Flight Control -- 6.6 Summary -- References -- Problems -- Chapter 7. Inertia Coupling and Spin -- 7.1 Introduction -- 7.2 Inertia Coupling -- 7.3 Autorotation of Wings and Fuselages -- 7.4 Airplane Spin -- 7.5 Equations of Motion for Steady-State Spin -- 7.6 Spin Recovery -- 7.7 Geometrical Modifications to Improve Spin Resistance -- 7.8 Summary -- References -- Problems -- Chapter 8. Stability and Control Problems at High Angles of Attack -- 8.1 Introduction -- 8.2 A Brief Historical Sketch -- 8.3 Brief Overview of High-Alpha Problems -- 8.4 Delta Wings at High Angles of Attack -- 8.5 Leading-Edge Extensions -- 8.6 Forebodies at High Angles of Attack -- 8.7 Relation Between Angle of Attack, Sideslip, and Roll Angle -- 8.8 Wing Rock -- 8.9 Roll Attractor of Delta Wings -- 8.10 Forebody-Induced Wing Rock -- 8.11 Suppression of Wing Rock -- 8.12 Roll Reversal and Yaw Departure -- 8.13 Control Concepts at High Angles of Attack -- 8.14 Summary -- References -- Appendix A. Standard Atmospheres -- Appendix B. Table of Laplace Transforms -- Appendix C. Cramer's Rule -- Appendix D. Conversion of U.S. Customary Units to SI Units -- Appendix E. Solved Examples -- Bibliography -- Index -- A -- B -- C -- D -- E -- F -- G -- H -- I -- J -- K -- L -- M -- N -- O -- P -- Q -- R -- S -- T -- U -- V -- W -- X -- Y -- Z.
588			_aDescription based on publisher supplied metadata and other sources.
590			_aElectronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
650		0	_aAirplanes -- Performance.
650		0	_aStability of airplanes.
650		0	_aAirplanes -- Control systems.
650		0	_aAerodynamics.
655		4	_aElectronic books.
776	0	8	_iPrint version: _aPamadi, Bandu N. _tPerformance, Stability, Dynamics, and Control of Airplanes _dReston : American Institute of Aeronautics and Astronautics,c2000 _z9781563475832
797	2		_aProQuest (Firm)
830		0	_aAIAA Education Series
856	4	0	_uhttps://ebookcentral.proquest.com/lib/orpp/detail.action?docID=3111614 _zClick to View
999			_c68281 _d68281