wing body alone configuration with a wing loading of W/S = 1000 N/m2 is flying in cruise condition at a speed of V=90 m/s at sea level. The zero lift pitching moment coefficient of the airplane is Cmac = Cm0 = -0.06 and the location of airplane aerodynamic center from te wing leading edge is Xac=0.25c. c - chord length. Distance of the CG of the aircraft Xcg from the wing leading edge is *
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Introduction to Aircraft Flight Mechanics
Introduction to Aircraft Flight Mechanics
Introduction to Aircraft Flight Mechanics:Performance, Static Stability, DynamicStability, and Classical Feedback Control
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Introduction to Aircraft Flight Mechanics:Performance, Static Stability, DynamicStability, and Classical Feedback ControlThomas R. YechoutwithSteven L. MorrisDavid E. BossertWayne F. HallgrenEDUCATION SERIESJoseph A. SchetzSeries Editor-in-ChiefVirginia Polytechnic Institute and State UniversityBlacksburg, VirginiaPublished byAmerican Institute of Aeronautics and Astronautics, Inc.1801 Alexander Bell Drive, Reston, VA 20191-4344
American Institute of Aeronautics and Astronautics, Inc., Reston, Virginia 12345Library of Congress Cataloging-in-Publication Data[CIP Data to come]Copyright # 2003 by the American Institute of Aeronautics and Astronautics, Inc. Thiswork was created in the performance of a Cooperative Research and DevelopmentAgreement with the Department of the Air Force. The Government of the United Stateshas certain rights to use this work.Data and information appearing in this book are for informational purposes only. AIAA isnot responsible for any injury or damage resulting from use or reliance, nor does AIAAwarrant that use or reliance will be free from privately owned rights.
AIAA Education Series Editor-in-Chief Joseph A. SchetzVirginia Polytechnic Institute and State University Editorial Board Daniel J. Biezad Robert G. LoewyCalifornia Polytechnic State Georgia Institute of Technology University Aaron R. Byerley Michael MohagheghU.S. Air Force Academy The Boeing Company Kajal K. Gupta Dora MusielakNASA Dryden Flight Research Northrop Grumman Corporation CenterJohn K. Harvey Conrad F. NewberryImperial College Naval Postgraduate School David K. Holger David K. SchmidtIowa State University University of Colorado, Colorado Springs Rakesk K. Kapania Peter TurchiVirginia Polytechnic Institute and Los Alamos National Laboratory State University Brian Landrum David M. Van WieUniversity of Alabama, Johns Hopkins University Huntsville
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ForewordIntroduction to Aircraft Flight Mechanics: Performance, Static Stability,Dynamic Stability, and Classical Feedback Control by Thomas R. Yechoutwith Steven L. Morris, David E. Bossert, and Wayne F. Hallgren as contribu-tors, all from the Department of Aeronautics of the U.S. Air Force Academy, isan outstanding textbook for use in undergraduate aeronautical engineeringcurricula. The text evolved from lecture notes at the Academy and it incorpo-rates many suggestions literally from hundreds of cadets to improve its peda-gogical value. The text reflects a wealth of experience by the authors. It coversall the essential topics needed to teach performance, static and dynamicstability, and classical feedback control of the aircraft at the introductory level. The ten chapters of this text cover the following topics: (1) Review of BasicAerodynamics, (2) Review of Basic Propulsion, (3) Aircraft Performance, (4)Aircraft Equations of Motion, (5) Aircraft Static Stability, (6) LinearizingEquations of Motion, (7) Aircraft Dynamic Stability, (8) Classical FeedbackControl, (9) Aircraft Stability and Control Augmentation, and (10) SpecialTopics (mainly additional analysis techniques for feedback control and thevarious types of aircraft flight control systems). This text should contributegreatly to the learning of the fundamental principles of flight mechanics that isthe crucial requirement in any aeronautical engineering curricula. The AIAA Education Series of textbooks and monographs, inaugurated in1984, embraces a broad spectrum of theory and application of different disci-plines in aeronautics and astronautics, including aerospace design practice. Theseries also includes texts on defense science, engineering, and management.These texts serve as teaching tools as well as reference materials for practicingengineers, scientists, and managers. The complete list of textbooks publishedin the series can be found on the end pages of this volume.J. S. PRZEMIENIECKIEditor-in-Chief (Retired)AIAA Education Series vii
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