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Perj'orman.ce, Stability, Dynamrcs, and Control of Aircraft by Bandu N. Pamadi
represents a novel approach of teaching an aeronautical engineering course as a
comprehensive and integrated exposure to several interrelated disciplines. The
text reflects many years of teaching experience of the author and his consul-
ting work as a senior research engineer with NASA Langley Research Center.
It contains all the necessary background material on aerodynamics, dynamics, and
control systems, discussing the fundamental principles with the use of sketches,
solved examples, and design exercises. It takes the reader from the early days of
the Wright Brothers to the modern era of combat aircraft flying at poststi:ll angles
of attack.
    Chapters 1 through 3 present basic princip,les of aerodynamics, aircraft perfor-
mance, and static equilibrium and control in steady flight.rChapter 4 deals with
aircraft dynamics aAd decoupled equations for lonYgitudinal and lateral motion,
and it intToduces the concept of stability derivatives. Chapter 5 discusses design
of stability augmentation systems and autopilots. Chapter"9'discusses aircraft res-
ponse and methods of closed-loop control of aircraft, while Chapters 7 and 8 dis-
guss problems ofinertial coupling, aircraft spin, and high angle of attack. A useful
feature of the text is the inclusion of solved examples presented to illustrate the
theory and basic principles involved.
      The Education Serie9 of textbooks and monographs published by the American
Institute of Aeronautics and Astronautics embraces a broad spec;rum of theory
and application of different disciplines in aeronautics and astronautics, including
aerospace design practice. The series also includes texts on defense science, engi-
neering, and management. The complete list of textbooks published in the series
(more than 50 titles) can be found a7the end of this volume. The series serves as
teaching texts as well as reference materials for pract.icing engineers, scientists.
and managers.
J. S. Przemieniecki
Editor-in-Chief
AIAA Education Series
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 Table of
Contents
Chapter 1.    Review of Basic Aerodynamic Pririciples   . . . . . . . . . . . . . .
   1.1   Introduction . - . . . . - . . - . . . i. . . . . . . . ~ - . . . - - . . . . . . . N .
    1.2 '  Fluid Flow over Wings and Bodies  . . . . - . . . . - . . . . . - ~ N . - * . .
   1.3  DragofBodies  .. . . . .. . - .. .. - N - - . .. . . - . . . . N . - .. . - - .
   1.4  WingParameters . - . . * ~ . . . * - . . . - . . . - . . - . . . - . . . . . . . . .
    1.5   Aerodynamic Characteristics ofWing Sections . . . . . . . . . . . . - . .
    1.6   Aerodynamic Characteristics ofFuute Wings . . . . . . . . - . . . . . . .
    1.7    Methods ofReducing Induced Drag  . . . . . . . . . . . . * . . . . . . . . .
     1.8    Tip Vortices: Formation and Hazards . .  - .  . . . . .  .  .  . . - . . . .  ~  N N .
    1.9   Flow ofa Compressible Fluid  . . . . . . . . . - * . . . . . . . - . . . . . . -
    1.10  Aerodynamic Fvorces in Supersonic Flow . . . . . . . . . . - - . . - - . * .
    1.11  Criticaf MachNumber  . . . . . - . . . . . . - . . . . - . . - . . . . . . . - . N
   1.12 AreaRule . . . . . . . . . . . . - . .... . . . .. . . . - . . . - .. - N . . ...
   1.13 Summary .,...... ... . - -... - .... ... . - . . ... -... ... -
         References . . . .. . - .. . . .. . - . . - . - . . .. - * - ~ . - . ~ . . . . . . .
         Problems  . . - . - . . . - . . . - . . - . . - . . . . - . - - . . . . . . . N . * . . -
Chapter 2.   Aircraft Performance  . - . . . . N . . . - . . . . . . . . . . . . . . . .
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