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Performance, Stability, Dynamics, and Control of Airplanes. (Record no. 68281)

MARC details
000 -LEADER
fixed length control field 05377nam a22004933i 4500
001 - CONTROL NUMBER
control field EBC3111614
003 - CONTROL NUMBER IDENTIFIER
control field MiAaPQ
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20240729124523.0
006 - FIXED-LENGTH DATA ELEMENTS--ADDITIONAL MATERIAL CHARACTERISTICS
fixed length control field m o d |
007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION
fixed length control field cr cnu||||||||
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 240724s2000 xx o ||||0 eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number 9781600860997
Qualifying information (electronic bk.)
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
Canceled/invalid ISBN 9781563475832
035 ## - SYSTEM CONTROL NUMBER
System control number (MiAaPQ)EBC3111614
035 ## - SYSTEM CONTROL NUMBER
System control number (Au-PeEL)EBL3111614
035 ## - SYSTEM CONTROL NUMBER
System control number (CaPaEBR)ebr10516719
035 ## - SYSTEM CONTROL NUMBER
System control number (OCoLC)922979020
040 ## - CATALOGING SOURCE
Original cataloging agency MiAaPQ
Language of cataloging eng
Description conventions rda
-- pn
Transcribing agency MiAaPQ
Modifying agency MiAaPQ
050 #4 - LIBRARY OF CONGRESS CALL NUMBER
Classification number TL671.4 -- .P28 2004eb
082 0# - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 629.13
100 1# - MAIN ENTRY--PERSONAL NAME
Personal name Pamadi, Bandu N.
245 10 - TITLE STATEMENT
Title Performance, Stability, Dynamics, and Control of Airplanes.
250 ## - EDITION STATEMENT
Edition statement 2nd ed.
264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE
Place of production, publication, distribution, manufacture Reston :
Name of producer, publisher, distributor, manufacturer American Institute of Aeronautics and Astronautics,
Date of production, publication, distribution, manufacture, or copyright notice 2000.
264 #4 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE
Date of production, publication, distribution, manufacture, or copyright notice ©2004.
300 ## - PHYSICAL DESCRIPTION
Extent 1 online resource (800 pages)
336 ## - CONTENT TYPE
Content type term text
Content type code txt
Source rdacontent
337 ## - MEDIA TYPE
Media type term computer
Media type code c
Source rdamedia
338 ## - CARRIER TYPE
Carrier type term online resource
Carrier type code cr
Source rdacarrier
490 1# - SERIES STATEMENT
Series statement AIAA Education Series
505 0# - FORMATTED CONTENTS NOTE
Formatted contents note Cover -- 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# - FORMATTED CONTENTS NOTE
Formatted contents note 5.9 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 ## - SOURCE OF DESCRIPTION NOTE
Source of description note Description based on publisher supplied metadata and other sources.
590 ## - LOCAL NOTE (RLIN)
Local note Electronic 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 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Airplanes -- Performance.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Stability of airplanes.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Airplanes -- Control systems.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Aerodynamics.
655 #4 - INDEX TERM--GENRE/FORM
Genre/form data or focus term Electronic books.
776 08 - ADDITIONAL PHYSICAL FORM ENTRY
Relationship information Print version:
Main entry heading Pamadi, Bandu N.
Title Performance, Stability, Dynamics, and Control of Airplanes
Place, publisher, and date of publication Reston : American Institute of Aeronautics and Astronautics,c2000
International Standard Book Number 9781563475832
797 2# - LOCAL ADDED ENTRY--CORPORATE NAME (RLIN)
Corporate name or jurisdiction name as entry element ProQuest (Firm)
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
Uniform title AIAA Education Series
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier <a href="https://ebookcentral.proquest.com/lib/orpp/detail.action?docID=3111614">https://ebookcentral.proquest.com/lib/orpp/detail.action?docID=3111614</a>
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