+612 9045 4394
 
CHECKOUT
$7.95 Delivery per order to Australia and New Zealand
100% Australian owned
Over a hundred thousand in-stock titles ready to ship
Performance, Stability, Dynamics and Control of Airplanes : AIAA Education Series - Bandu N. Pamadi

Performance, Stability, Dynamics and Control of Airplanes

AIAA Education Series

Hardcover Published: 31st January 2004
ISBN: 9781563475832
Number Of Pages: 768

Share This Book:

Hardcover

RRP $410.99
$284.50
31%
OFF
or 4 easy payments of $71.13 with Learn more
Ships in 10 to 15 business days

Earn 569 Qantas Points
on this Book

This book provides a comprehensive and integrated exposure to airplane performance, stability, dynamics, and flight control. It supports a two-semester course for senior undergraduate or first-year graduate students in aerospace engineering. Basic aerodynamics, dynamics, and linear control systems are presented to help the reader grasp the main subject matter. 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, MATLAB tools are used for the control design. In the second edition, lists of symbols/nomenclature and tables of important formulas are included to facilitate the reader.

Prefacep. xv
Preface to the Previous Editionp. xvii
Review of Basic Aerodynamic Principlesp. 1
Introductionp. 1
Fluid Flow over Wings and Bodiesp. 2
Drag of Bodiesp. 11
Wing Parametersp. 12
Aerodynamic Characteristics of Wing Sectionsp. 18
Aerodynamic Characteristics of Finite Wingsp. 27
Methods of Reducing Induced Dragp. 31
Tip Vortices: Formation and Hazardsp. 32
Flow of a Compressible Fluidp. 35
Aerodynamic Forces in Supersonic Flowp. 36
Critical Mach Numberp. 40
Area Rulep. 59
Summaryp. 64
Referencesp. 65
Problemsp. 66
Aircraft Performancep. 67
Introductionp. 67
Equations of Motion for Flight in Vertical Planep. 70
Gliding Flightp. 73
Level Flightp. 81
Climbing Flightp. 94
Range and Endurancep. 106
Endurancep. 114
Turning Flightp. 122
Takeoff and Landingp. 146
Hazards During Takeoff and Landing: Windshear and Microburstp. 156
Summaryp. 158
Referencesp. 158
Problemsp. 159
Static Stability and Controlp. 165
Introductionp. 165
Concept of Equilibrium and Stabilityp. 165
Static Longitudinal Stabilityp. 168
Stability in Maneuvering Flightsp. 249
Static Directional Stabilityp. 259
Lateral Stabilityp. 294
Summaryp. 313
Referencesp. 313
Problemsp. 314
Equations of Motion and Estimation of Stability Derivativesp. 321
Introductionp. 321
Axes Systemsp. 322
Equations of Motion and Concept of Moving Axes Systemp. 361
Estimation of Stability Derivativesp. 391
Summaryp. 438
Referencesp. 439
Problemsp. 440
Linear Systems, Theory, and Design: A Brief Reviewp. 443
Introductionp. 443
Laplace Transformp. 444
Transfer Functionp. 449
System Responsep. 450
Steady-State Errors of Unity Feedback Systemsp. 457
Frequency Responsep. 460
Stability of Closed-Loop Systemsp. 464
Relations Between Time-Domain and Frequency-Domain Parametersp. 488
Design of Compensatorsp. 491
State-Space Analysis and Designp. 510
Summaryp. 536
Referencesp. 536
Problemsp. 536
Airplane Response and Closed-Loop Controlp. 541
Introductionp. 541
Longitudinal Responsep. 541
Lateral-Directional Responsep. 569
Flying Qualitiesp. 595
Closed-Loop Flight Controlp. 599
Summaryp. 626
Referencesp. 627
Problemsp. 627
Inertia Coupling and Spinp. 631
Introductionp. 631
Inertia Couplingp. 631
Autorotation of Wings and Fuselagesp. 644
Airplane Spinp. 650
Equations of Motion for Steady-State Spinp. 653
Spin Recoveryp. 667
Geometrical Modifications to Improve Spin Resistancep. 668
Summaryp. 674
Referencesp. 675
Problemsp. 676
Stability and Control Problems at High Angles of Attackp. 677
Introductionp. 677
A Brief Historical Sketchp. 677
Brief Overview of High-Alpha Problemsp. 678
Delta Wings at High Angles of Attackp. 680
Leading-Edge Extensionsp. 690
Forebodies at High Angles of Attackp. 694
Relation Between Angle of Attack, Sideslip, and Roll Anglep. 699
Wing Rockp. 699
Roll Attractor of Delta Wingsp. 714
Forebody-Induced Wing Rockp. 718
Suppression of Wing Rockp. 729
Roll Reversal and Yaw Departurep. 736
Control Concepts at High Angles of Attackp. 739
Summaryp. 753
Referencesp. 754
Standard Atmospheresp. 757
Table of Laplace Transformsp. 761
Cramer's Rulep. 763
Conversion of U.S. Customary Units to SI Unitsp. 765
Solved Examplesp. 767
Bibliographyp. 769
Indexp. 771
Series Listingp. 781
Table of Contents provided by Rittenhouse. All Rights Reserved.

ISBN: 9781563475832
ISBN-10: 1563475839
Series: AIAA Education Series
Audience: Professional
Format: Hardcover
Language: English
Number Of Pages: 768
Published: 31st January 2004
Publisher: American Institute of Aeronautics & Astronautics
Country of Publication: US
Dimensions (cm): 23.0 x 16.51  x 4.45
Weight (kg): 1.43
Edition Number: 2
Edition Type: Revised

Earn 569 Qantas Points
on this Book