Introduction To Aircraft Flight Mechanics


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Introduction to Aircraft Flight Mechanics


Introduction to Aircraft Flight Mechanics

Author: Thomas R. Yechout

language: en

Publisher: AIAA

Release Date: 2003


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Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.

Introduction to Aircraft Flight Dynamics


Introduction to Aircraft Flight Dynamics

Author: Louis V. Schmidt

language: en

Publisher: AIAA

Release Date: 1998


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Fundamentals of Airplane Flight Mechanics


Fundamentals of Airplane Flight Mechanics

Author: David G. Hull

language: en

Publisher: Springer Science & Business Media

Release Date: 2007-01-20


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Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This text is concerned with the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane. Algorithms are presented for calculating lift, drag, pitching moment, and stability derivatives. Flight mechanics is a discipline. As such, it has equations of motion, acceptable approximations, and solution techniques for the approximate equations of motion. Once an analytical solution has been obtained, numbers are calculated in order to compare the answer with the assumptions used to derive it and to acquaint students with the sizes of the numbers. A subsonic business jet is used for these calculations.