FUNDAMENTALS OF AIRCRAFT FLIGHT MECHANICS: Aerodynamics, Performance, Stability and Control for Aerospace Engineering Students
Language: English
Published by Independently published, 2026
- Softcover
- New

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- Title
- FUNDAMENTALS OF AIRCRAFT FLIGHT MECHANICS: Aerodynamics, Performance, Stability and Control for Aerospace Engineering Students
- Author
- Calder, Ethan R.; Technical Press, AeroVector
- Publisher
- Independently published
- Publication year
- 2026
- Condition
- New
- Binding
- Soft cover
- Language
- English
- ISBN 13
- 9798191002880
A formula memorised without its assumptions cannot tell you when it stops applying. In flight mechanics, knowing the limits of a model matters just as much as knowing the model itself.
Aircraft flight mechanics is where aerodynamics, propulsion, performance, stability, control, and rigid-body motion come together. It is also where many students become frustrated by compressed derivations, unfamiliar notation, unexplained approximations, and formulas presented without enough physical meaning.
Fundamentals of Aircraft Flight Mechanics takes a clearer and more rigorous approach.
Instead of asking you to memorise equations, this book shows where they come from, what assumptions they depend on, how they are applied, and when they should no longer be trusted. Intermediate steps remain visible, variables are defined consistently, approximations are explained, and worked examples include complete unit tracking.
Across sixteen structured chapters, you will progress from atmospheric properties and airspeed measurement to aircraft performance, stability analysis, dynamic modes, feedback augmentation, and autopilot fundamentals.
Inside this book, you will learn how to:
- Build and interpret thrust-required and power-required curves
- Explain minimum-drag speed, minimum-power speed, and the region of reversed command
- Calculate climb angle, rate of climb, ceilings, glide performance, range, and endurance
- Compare jet and propeller aircraft performance under changing weight, altitude, and wind conditions
- Construct a flight envelope and determine stall limits, corner speed, gust loads, and structural boundaries
- Distinguish between instantaneous and sustained turn performance
- Calculate takeoff and landing performance using clearly stated assumptions
- Derive and interpret the six-degree-of-freedom equations of motion
- Determine neutral point, static margin, trim requirements, and centre-of-gravity limits
- Understand lateral and directional stability, including dihedral effect, weathercock stability, rudder control, and adverse yaw
- Identify the short-period, phugoid, roll subsidence, spiral, and Dutch roll modes
- Examine how pitch dampers, yaw dampers, roll dampers, and washout filters modify aircraft response
Every chapter includes learning objectives, carefully developed theory, worked examples, practice problems, answer checks, key equations, and concise summaries.
The back matter adds a detailed list of symbols, glossary, standard-atmosphere tables, unit conversions, physical constants, representative aircraft data, and answers to selected problems.
This book is written for aerospace and aeronautical engineering students, graduate engineers entering flight test or controls work, technically inclined pilots, instructors, and independent learners seeking a structured path into flight mechanics.
Build the subject from first principles, follow every step, and gain the confidence to understand what an aircraft will do and why. Get your copy today and master aircraft flight mechanics from atmosphere to autopilot.
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