Flight-velocity, Etc
Author | : |
Publisher | : |
Total Pages | : 190 |
Release | : 1906 |
Genre | : Flight |
ISBN | : |
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Author | : |
Publisher | : |
Total Pages | : 190 |
Release | : 1906 |
Genre | : Flight |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : |
Release | : 1899 |
Genre | : Flight |
ISBN | : |
Author | : Arnold Samuelson |
Publisher | : |
Total Pages | : 68 |
Release | : 1906 |
Genre | : Aerodynamics |
ISBN | : |
Author | : Albert Storace |
Publisher | : CRC Press |
Total Pages | : 85 |
Release | : 2023-12-04 |
Genre | : Technology & Engineering |
ISBN | : 1003820999 |
The Physics of Flight provides a comprehensive explanatory reference on the basic physics of flight with a clear presentation of the underlying mathematics. It presents a momentum-based explanation of lift making no use of Bernoulli’s theorem. Misconceptions are disproved, such as identifying centrifugal force experienced in an airplane undergoing maneuvers as a fictitious force, and not attributing weightlessness during airplane pitch over or experienced in an airplane performing a parabolic flight path to the effects of free fall. This book places particular emphasis on Newton’s second law of motion to explain the effects of forces acting on an airplane, the mechanism of lift, and the principles of propulsion. This book is intended for undergraduate aviation and aerospace students taking courses in Flight Dynamics, Introduction to Flight, and Physics of Flight.
Author | : Richard Von Mises |
Publisher | : Courier Corporation |
Total Pages | : 680 |
Release | : 1959-01-01 |
Genre | : Technology & Engineering |
ISBN | : 9780486605418 |
Coverage of fundamental fluid dynamics includes practical and theoretical examinations of aeronautical engineering, stability, imcompressible fluids, and wing design
Author | : Frederick William Lanchester |
Publisher | : |
Total Pages | : 476 |
Release | : 1918 |
Genre | : Aerodynamics |
ISBN | : |
Author | : Charlie M. Jackson |
Publisher | : |
Total Pages | : 36 |
Release | : 1966 |
Genre | : Aeronautics |
ISBN | : |
An approximate method for calculating climb and acceleration performance of an air-breathing aircraft has been developed. Basically, the method involves linearization of the equations of motion to obtain closed-form expressions for the desired performance parameters. These expressions are applied over finite velocity intervals where the aerodynamic, propulsion, and flight-path parameters are assumed to be constant. The method is extended by a rapidly convergent iteration procedure to estimate the climb performance for a flight path limited by sonic-boom considerations. Typical examples are presented where the performance is estimated for an air-breathing boost mission to hypersonic speeds and for a complete supersonic-transport mission. The examples illustrate the simplicity of the method and show that the estimated performance is in good agreement with the results of a numerical integration of the equations of motion. The application of the approximate method to these examples indicates the utility of the method for producing performance estimates suitable for preliminary airframe design, sizing studies, propulsion-system evaluation, and cursory heat-transfer and inlet-flow-field determinations along a flight path. In order to increase the utility of the method further, nomograms are presented which provide rapid solutions to the approximate performance equations.
Author | : |
Publisher | : |
Total Pages | : 762 |
Release | : 1967 |
Genre | : Airplanes |
ISBN | : |
Author | : United States. Army Materiel Command |
Publisher | : |
Total Pages | : 116 |
Release | : 1965 |
Genre | : Aerodynamics |
ISBN | : |
Author | : Angelo Miele |
Publisher | : Courier Dover Publications |
Total Pages | : 436 |
Release | : 2016-03-15 |
Genre | : Technology & Engineering |
ISBN | : 0486801462 |
Classic text analyzes trajectories of aircraft, missiles, satellites, and spaceships in terms of gravitational forces, aerodynamic forces, and thrust. Topics include general principles of kinematics, dynamics, aerodynamics, propulsion; quasi-steady and non-steady flight; and applications. 1962 edition.