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Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control (AIAA Education) [Hardcover]

Thomas R. Yechout (Author), Steven L. Morris (Author), David E. Bossert (Author)
5.0 out of 5 stars  See all reviews (3 customer reviews)

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Book Description

May 2003 1563475774 978-1563475771 First Edition
This textbook is based on a 15-year successful approach to teaching aircraft flight mechanics at the U.S. Air Force Academy. It explains all the concepts and derivations of equations for aircraft flight mechanics. It covers; aircraft performance, static stability, aircraft dynamics stability, and feedback control. The chapters present real world applications and contain problems. Each year the Academy's students are placed with industry, NASA, and Air Force labs and test organizations, and the student reviews are outstanding, illustrating the quality of the author's approach.

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Product Details

  • Hardcover: 649 pages
  • Publisher: AIAA (American Institute of Aeronautics & Ast; First Edition edition (May 2003)
  • Language: English
  • ISBN-10: 1563475774
  • ISBN-13: 978-1563475771
  • Product Dimensions: 9.1 x 7.1 x 1.4 inches
  • Shipping Weight: 2.3 pounds (View shipping rates and policies)
  • Average Customer Review: 5.0 out of 5 stars  See all reviews (3 customer reviews)
  • Amazon Best Sellers Rank: #548,960 in Books (See Top 100 in Books)

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4 of 5 people found the following review helpful:
5.0 out of 5 stars Excellent Flight Mechanics Book!!, September 26, 2006
By 
Calvin Walker (Columbus, MS USA) - See all my reviews
(REAL NAME)   
This review is from: Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control (AIAA Education) (Hardcover)
This is by far one of the best written books on flight mechanics. Actually, it so good that I plan to teach a aircraft stability and control course using this book.
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1 of 1 people found the following review helpful:
5.0 out of 5 stars Amazing..., August 19, 2010
This review is from: Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control (AIAA Education) (Hardcover)
Dr. Yechout was my professor at the US Air Force Academy and I have to say that after nearly a decade since this course, I still remember how enjoyable the course and book were. The equations are laid out in simple, easy to understand approach that would be valuable to any student.
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1 of 1 people found the following review helpful:
5.0 out of 5 stars Easily Understanding, May 5, 2008
This review is from: Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control (AIAA Education) (Hardcover)
This book is suitable to anyone who is interested in this field. If you understand the knowledge within this book, then it's easier for you to read any more complicated contents. Highly recommended!!
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Inside This Book (learn more)
First Sentence:
Lift, drag, thrust, and weight are the four primary forces acting on an aircraft in flight (refer to Fig. 1.1). Read the first page
Key Phrases - Statistically Improbable Phrases (SIPs): (learn more)
earth axis system, body axis system, longitudinal flight control system, right engine failure, asymptote centroid, vertical tail contribution, positive roll rate, corrected rpm, stability axis system, rate feedback system, dynamic stability characteristics, positive sideslip angle, phugoid roots, parabolic input, positive rudder deflection, real axis location, positive rolling moment, short period roots, short period damping ratio, negative rolling moment, max overshoot, unit ramp input, damping derivative, corrected properties, aircraft equations
Key Phrases - Capitalized Phrases (CAPs): (learn more)
Lear Jet, Combining Eqs, New York, Actuator Fig, Actuator Aircraft, Air Force Flight Test Center, Education Series, Historical Snapshot-The, Design Perspective, Body Therefore, Laminar Turbulent
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