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Author : Bandu N. Pamadi
Publisher : AIAA
Page : 810 pages
File Size : 43,7 Mb
Release : 2004
Category : Aerodynamics
ISBN : 1600860990
Author : Bandu N. Pamadi
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 816 pages
File Size : 49,6 Mb
Release : 2004
Category : Science
ISBN : UOM:39015058114557
This book provides a comprehensive and integrated exposure to airplane performance, stability, dynamics, and flight control. The text supports a two-semester course for senior undergraduate or first-year graduate students in aerospace engineering. Basic aerodynamics, dynamics, and linear control systems are presented to help the reader grasp the main subject matter. In this text, the airplane is assumed to be a rigid body-elastic deformations and their effects on airplane motion are not considered. Numerous solved examples illustrate theory and design methods. Several exercise problems with answers are included in each chapter to help the reader acquire problem-solving skills. In addition, MATLAB tools are used for the control design. Professors! To receive your solutions manual, e-mail your request and full address to [email protected].
Author : Courtland D. Perkins,Robert E. Hage
Publisher : Unknown
Page : 0 pages
File Size : 53,5 Mb
Release : 1956
Category : Electronic
ISBN : OCLC:1411582521
Author : Courtland D. Perkins,Robert E. Hage
Publisher : John Wiley & Sons
Page : 512 pages
File Size : 48,6 Mb
Release : 1949-01-15
Category : Science
ISBN : WISC:89090518713
First written in 1949, this is a classic text in aeronautical engineering. It covers airplane performance in reciprocating engine craft, propeller performance, as well as aircraft stability and control. This is an excellent book for the professional and the serious amateur aircraft maker. It is written in a straightforward and easy to understand manner. To get the most out of this book, readers should have an understanding of differential calculus.
Author : Robert C. Nelson
Publisher : WCB/McGraw-Hill
Page : 441 pages
File Size : 44,7 Mb
Release : 1998
Category : Aerodynamique / Aeronautique / Aerospatial / Automatique / Avion / Commande / Conception / Controle / Navigation / Stabilite
ISBN : 0071158383
The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Author : Robert F. Stengel
Publisher : Princeton University Press
Page : 914 pages
File Size : 54,5 Mb
Release : 2022-11-01
Category : Science
ISBN : 9780691237046
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 : Louis V. Schmidt
Publisher : AIAA
Page : 426 pages
File Size : 51,7 Mb
Release : 1998
Category : Aerodynamics
ISBN : 160086077X
Author : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 47,7 Mb
Release : 2003
Category : Aerodynamics
ISBN : 1600860788
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 : Edward Seckel
Publisher : Academic Press
Page : 522 pages
File Size : 55,6 Mb
Release : 2014-05-10
Category : Technology & Engineering
ISBN : 9781483220154
Stability and Control of Airplanes and Helicopters deals with aircraft flying qualities that determine the stability and control of airplanes and helicopters. It includes problems based on real aircraft, selected to represent the gamut from simple to complicated, and from conventional utility designs to futuristic research types. Many of these problems involve comparison of theory and experiment to demonstrate their mutual relationship. Comprised of 25 chapters, this book begins with a discussion on the aerodynamics of the component parts related to the lift and moment characteristics of an airplane, including wings and associated accessories; bodies such as fuselages, nacelles, and tip tanks; and control surfaces. The reader is then introduced to some mathematical techniques for linear differential equations; steady flight at different speeds; and stick force and control-free stability. Subsequent chapters focus on flaps and high-lift devices; power and compressibility effects; and the manner in which the aircraft responds to the application of control. Aeroelasticity and longitudinal equations of motion are also examined. This monograph is intended for undergraduate and graduate students taking modern engineering courses.
Author : Jan Roskam,Chuan-Tau Edward Lan
Publisher : DARcorporation
Page : 748 pages
File Size : 43,7 Mb
Release : 1997
Category : Science
ISBN : 1884885446
Author : Jan Roskam
Publisher : DARcorporation
Page : 612 pages
File Size : 48,8 Mb
Release : 1998
Category : Science
ISBN : 1884885179
Author : Pascual Marqués,Andrea Da Ronch
Publisher : John Wiley & Sons
Page : 776 pages
File Size : 40,7 Mb
Release : 2017-04-19
Category : Technology & Engineering
ISBN : 9781118928714
Comprehensively covers emerging aerospace technologies Advanced UAV aerodynamics, flight stability and control: Novel concepts, theory and applications presents emerging aerospace technologies in the rapidly growing field of unmanned aircraft engineering. Leading scientists, researchers and inventors describe the findings and innovations accomplished in current research programs and industry applications throughout the world. Topics included cover a wide range of new aerodynamics concepts and their applications for real world fixed-wing (airplanes), rotary wing (helicopter) and quad-rotor aircraft. The book begins with two introductory chapters that address fundamental principles of aerodynamics and flight stability and form a knowledge base for the student of Aerospace Engineering. The book then covers aerodynamics of fixed wing, rotary wing and hybrid unmanned aircraft, before introducing aspects of aircraft flight stability and control. Key features: Sound technical level and inclusion of high-quality experimental and numerical data. Direct application of the aerodynamic technologies and flight stability and control principles described in the book in the development of real-world novel unmanned aircraft concepts. Written by world-class academics, engineers, researchers and inventors from prestigious institutions and industry. The book provides up-to-date information in the field of Aerospace Engineering for university students and lecturers, aerodynamics researchers, aerospace engineers, aircraft designers and manufacturers.
Author : John T. Lowry
Publisher : AIAA
Page : 508 pages
File Size : 45,7 Mb
Release : 1999
Category : Mathematics
ISBN : 1563473305
Pilots, aviation students, kitplane builders, aircraft fleet operators and aeronautical engineers can all determine how their propeller-driven airplanes will perform, under any conditions, by using the step-by-step bootstrap approach introduced in this book. A few routine flying manoeuvres (climbs, glides, a level speed run) will give the necessary nine numbers. High-school level calculations then give performance numbers with much greater detail and accuracy than many other methods - for the reader's individual aircraft.
Author : Malcolm J. Abzug,E. Eugene Larrabee
Publisher : Cambridge University Press
Page : 128 pages
File Size : 43,9 Mb
Release : 2002-09-23
Category : Technology & Engineering
ISBN : 9781107320192
From the early machines to today's sophisticated aircraft, stability and control have always been crucial considerations. In this second edition, Abzug and Larrabee again forge through the history of aviation technologies to present an informal history of the personalities and the events, the art and the science of airplane stability and control. The book includes never-before-available impressions of those active in the field, from pre-Wright brothers airplane and glider builders through to contemporary aircraft designers. Arranged thematically, the book deals with early developments, research centers, the effects of power on stability and control, the discovery of inertial coupling, the challenge of stealth aerodynamics, a look toward the future, and much more. It is profusely illustrated with photographs and figures, and includes brief biographies of noted stability and control figures along with a core bibliography. Professionals, students, and aviation enthusiasts alike will appreciate this readable history of airplane stability and control.
Author : Ralph D. Kimberlin
Publisher : AIAA
Page : 464 pages
File Size : 40,8 Mb
Release : 2003
Category : Airplanes
ISBN : 1600860567
Annotation The measurement of performance during an airplane's flight, testing is one of the more important tasks to be accomplished during its development as it impacts on both the airplane's safety and its marketability. This book discusses performance for both propeller-driven and jet aircraft.