This book presents flight mechanics of aircraft, spacecraft, and rockets to technical and non-technical readers in simple terms and based purely on physical principles. Adapting an accessible and lucid writing style, the book retains the scientific authority and conceptual substance of an engineering textbook without requiring a background in physics or engineering mathematics. Professor Tewari explains relevant physical principles of flight by straightforward examples and meticulous diagrams and figures. Important aspects of both atmospheric and space flight mechanics are covered, including performance, stability and control, aeroelasticity, orbital mechanics, and altitude control. The book describes airplanes, gliders, rotary wing and flapping wing flight vehicles, rockets, and spacecraft and visualizes the essential principles using detailed illustration. It is an ideal resource for managers and technicians in the aerospace industry without engineering degrees, pilots, and anyone interested in the mechanics of flight.
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.
In addition, the volume presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. Throughout, a subsonic business jet is used as an example for the calculations presented in the book.
AIRCRAFT This chapter treats the aerodynamics of helicopters and aircraft designed to take off in a very short distance , or even vertically . Such aircraft are known as V / STOL aircraft , an acronym denoting vertical or short takeoff ...
This book provides extensive coverage of individual topics within flight mechanics, including overviews of aerodynamics and propulsion.
Designed for courses in aerodynamics, aeronautics and flight mechanics, this text examines the aerodynamics, propulsion, performance, stability and control of an aircraft.
Classic text analyzes trajectories of aircraft, missiles, satellites, and spaceships in terms of gravitational forces, aerodynamic forces, and thrust.
Covers all aspects of flight performance of modern day high-performance aircraft.
Now updated and expanded, this authoritative book by award-winning aeronautics engineer Robert Stengel presents traditional material in the context of modern computational tools and multivariable methods.
In contrast, Elementary Flight Dynamics with an Introduction to Bifurcation and Continuation Methods uses an optimal mix of physical insight and mathematical presentatio
Hajiyev Ch . and Caliskan F. Fault Diagnosis and Reconfiguration in Flight Control Systems , Kluwer Academic ... feedback design : Concepts for a classical / modern synthesis , IEEE Transactions on Automatic Control , Ac - 26 ( 1 ) ...