Scientific and Technical Aerospace Reports
Author :
Publisher :
Page : 702 pages
File Size : 20,81 MB
Release : 1995
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 702 pages
File Size : 20,81 MB
Release : 1995
Category : Aeronautics
ISBN :
Author : Eric T. Falangas
Publisher : John Wiley & Sons
Page : 432 pages
File Size : 40,59 MB
Release : 2015-12-03
Category : Technology & Engineering
ISBN : 1119134870
The purpose of this book is to assist analysts, engineers, and students toward developing dynamic models, and analyzing the control of flight vehicles with various blended features comprising aircraft, launch vehicles, reentry vehicles, missiles and aircraft. Graphical methods for analysing vehicle performance Methods for trimming deflections of a vehicle that has multiple types of effectors Presents a parameters used for speedily evaluating the performance, stability, and controllability of a new flight vehicle concept along a trajectory or with fixed flight conditions
Author : Robert C. Nelson
Publisher :
Page : 464 pages
File Size : 49,96 MB
Release : 1998
Category : History
ISBN :
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author :
Publisher :
Page : 538 pages
File Size : 38,4 MB
Release : 1991
Category : Aeronautics
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Author :
Publisher :
Page : 654 pages
File Size : 45,86 MB
Release : 1992
Category : Aeronautics
ISBN :
Author : Josef Rom
Publisher : Springer Science & Business Media
Page : 408 pages
File Size : 24,26 MB
Release : 2012-12-06
Category : Science
ISBN : 1461228247
The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perform well at very high incidence, near and beyond stall. However, a comprehensive presentation of the methods and results applicable to the studies of the complex aerodynamics at high angle of attack has not been covered in monographs or textbooks. This book is not the usual textbook in that it goes beyond just presenting the basic theoretical and experimental know-how, since it contains reference material to practical calculation methods and technical and experimental results which can be useful to the practicing aerospace engineers and scientists. It can certainly be used as a text and reference book for graduate courses on subjects related to high angles of attack aerodynamics and for topics related to three-dimensional separation in viscous flow courses. In addition, the book is addressed to the aerodynamicist interested in a comprehensive reference to methods of analysis and computations of high angle of attack flow phenomena and is written for the aerospace scientist and engineer who is familiar with the basic concepts of viscous and inviscid flows and with computational methods used in fluid dynamics.
Author : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 12,80 MB
Release : 2003
Category : Aerodynamics
ISBN : 9781600860782
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.
Author :
Publisher :
Page : 388 pages
File Size : 24,24 MB
Release : 1981
Category : Aeronautics
ISBN :
Author : Robert F. Stengel
Publisher : Princeton University Press
Page : 914 pages
File Size : 26,72 MB
Release : 2022-11-01
Category : Science
ISBN : 0691237042
An updated and expanded new edition of an authoritative book on flight dynamics and control system design for all types of current and future fixed-wing aircraft Since it was first published, Flight Dynamics has offered a new approach to the science and mathematics of aircraft flight, unifying principles of aeronautics with contemporary systems analysis. 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. Special attention is devoted to models and techniques for analysis, simulation, evaluation of flying qualities, and robust control system design. Using common notation and not assuming a strong background in aeronautics, Flight Dynamics will engage a wide variety of readers, including aircraft designers, flight test engineers, researchers, instructors, and students. It introduces principles, derivations, and equations of flight dynamics as well as methods of flight control design with frequent reference to MATLAB functions and examples. Topics include aerodynamics, propulsion, structures, flying qualities, flight control, and the atmospheric and gravitational environment. The second edition of Flight Dynamics features up-to-date examples; a new chapter on control law design for digital fly-by-wire systems; new material on propulsion, aerodynamics of control surfaces, and aeroelastic control; many more illustrations; and text boxes that introduce general mathematical concepts. Features a fluid, progressive presentation that aids informal and self-directed study Provides a clear, consistent notation that supports understanding, from elementary to complicated concepts Offers a comprehensive blend of aerodynamics, dynamics, and control Presents a unified introduction of control system design, from basics to complex methods Includes links to online MATLAB software written by the author that supports the material covered in the book
Author :
Publisher :
Page : 648 pages
File Size : 36,21 MB
Release : 1992
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ISBN :