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Author: A. G. Panaras
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781600869167
Category : Aerodynamics
Languages : en
Pages : 0
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Book Description
In "Aerodynamic Principles of Flight Vehicles" Argyris Panaras examines the fundamentals of vortices and shock waves, aerodynamic estimation of lift and drag, airfoil theory, boundary layer control, and high-speed, high-temperature flow. Individual chapters address vortices in aerodynamics, transonic and supersonic flows, transonic/supersonic aircraft configurations, and high-supersonic/hypersonic flows, beginning with definitions and historical data, and then describing present-day status and current research challenges. Emphasis is given to flow control, to the evolution of flight vehicle shapes as flight speed has increased, and to discoveries that enabled breakthrough developments in flight. The book: examines why various equations and technologies were developed, explains major contributors in areas such as vortices and aircraft wakes, drag buildup, sonic boom, and shock wave-boundary layer interactions, among others, and helps readers apply concepts from the material to their own projects. Archival and encyclopedic, "Aerodynamic Principles of Flight Vehicles" is a superb reference for aeronautical students and professionals alike. Although most beneficial to readers with a working knowledge of aerodynamics, it is accessible to anyone with an introductory understanding of the field.
Author: A. G. Panaras
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781600869167
Category : Aerodynamics
Languages : en
Pages : 0
Get Book
Book Description
In "Aerodynamic Principles of Flight Vehicles" Argyris Panaras examines the fundamentals of vortices and shock waves, aerodynamic estimation of lift and drag, airfoil theory, boundary layer control, and high-speed, high-temperature flow. Individual chapters address vortices in aerodynamics, transonic and supersonic flows, transonic/supersonic aircraft configurations, and high-supersonic/hypersonic flows, beginning with definitions and historical data, and then describing present-day status and current research challenges. Emphasis is given to flow control, to the evolution of flight vehicle shapes as flight speed has increased, and to discoveries that enabled breakthrough developments in flight. The book: examines why various equations and technologies were developed, explains major contributors in areas such as vortices and aircraft wakes, drag buildup, sonic boom, and shock wave-boundary layer interactions, among others, and helps readers apply concepts from the material to their own projects. Archival and encyclopedic, "Aerodynamic Principles of Flight Vehicles" is a superb reference for aeronautical students and professionals alike. Although most beneficial to readers with a working knowledge of aerodynamics, it is accessible to anyone with an introductory understanding of the field.
Author: Ashish Tewari
Publisher: Springer
ISBN: 3319300229
Category : Technology & Engineering
Languages : en
Pages : 136
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Book Description
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.
Author: Holt Ashley
Publisher: Addison Wesley Publishing Company
ISBN:
Category : Science
Languages : en
Pages : 408
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Book Description
Author: Frederick O. Smetana
Publisher: AIAA
ISBN: 9781600860577
Category : Aerodynamics
Languages : en
Pages : 392
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Book Description
Annotation "Flight Vehicle Performance and Aerodynamic Control is designed to serve as a text for either an 11-week or a 16-week course at the sophomore level. It explains typical methods used to estimate aircraft performance, the theoretical basis of these methods, and how various parameters derived from the aircraft geometry can be used to estimate the requirements of control surfaces and the aerodynamic forces required to actuate these surfaces. This book includes time-tested computer programs that perform the analyses in a manner that reduces student error and improves result accuracy. Because the source code is given, users with a FORTRAN compiler can modify the program to suit particular needs. The major advantage of the software is that more realistic problems may be treated and the effects of parametric programs are more accurate than calculators. The programs are available as executables for Windows machines as well as in ASCII source code versions that can be readily compiled and then executed on Unix, Linux, and Macintosh machines and on mainframes.
Author: Mark Drela
Publisher: MIT Press
ISBN: 0262319934
Category : Science
Languages : en
Pages : 304
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Book Description
An overview of the physics, concepts, theories, and models underlying the discipline of aerodynamics. This book offers a general overview of the physics, concepts, theories, and models underlying the discipline of aerodynamics. A particular focus is the technique of velocity field representation and modeling via source and vorticity fields and via their sheet, filament, or point-singularity idealizations. These models provide an intuitive feel for aerodynamic flow-field behavior and are the basis of aerodynamic force analysis, drag decomposition, flow interference estimation, and other important applications. The models are applied to both low speed and high speed flows. Viscous flows are also covered, with a focus on understanding boundary layer behavior and its influence on aerodynamic flows. The book covers some topics in depth while offering introductions and summaries of others. Computational methods are indispensable for the practicing aerodynamicist, and the book covers several computational methods in detail, with a focus on vortex lattice and panel methods. The goal is to improve understanding of the physical models that underlie such methods. The book also covers the aerodynamic models that describe the forces and moments on maneuvering aircraft, and provides a good introduction to the concepts and methods used in flight dynamics. It also offers an introduction to unsteady flows and to the subject of wind tunnel measurements. The book is based on the MIT graduate-level course “Flight Vehicle Aerodynamics” and has been developed for use not only in conventional classrooms but also in a massive open online course (or MOOC) offered on the pioneering MOOC platform edX. It will also serve as a valuable reference for professionals in the field. The text assumes that the reader is well versed in basic physics and vector calculus, has had some exposure to basic fluid dynamics and aerodynamics, and is somewhat familiar with aerodynamics and aeronautics terminology.
Author: R. H. Barnard
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 388
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Book Description
This book is intended to provide a description on the principles of aircraft flight in physical rather than mathematical terms. The authors have included some of the more important practical aspects of aircraft flight plus examples of innovations, descriptions of which are generally only found scattered in assorted technical journals. two simple formulae as a means of defining important terms such as lift coefficient and Reynolds number, which are essential to the understanding of aeronautics. important, or interesting. They have also restricted coverage to the aerodynamics and mechanics of flight, with only a brief consideration of other aspects such as structural influences. interested in aircraft or contemplating a career in aeronautics. Students of aeronautical engineering should find it helpful as introductory and background reading. It should also be useful to employees in the industry such as flight crew and ground staff. physical science and is at least vaguely familiar with concepts such as energy and momentum.
Author: Michael V. Cook
Publisher: Butterworth-Heinemann
ISBN: 008098486X
Category : Science
Languages : en
Pages : 400
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Book Description
Flight dynamicists today need not only a thorough understanding of the classical stability and control theory of aircraft, but also a working appreciation of flight control systems and consequently a grounding in the theory of automatic control. In this text the author fulfils these requirements by developing the theory of stability and control of aircraft in a systems context. The key considerations are introduced using dimensional or normalised dimensional forms of the aircraft equations of motion only and through necessity the scope of the text will be limited to linearised small perturbation aircraft models. The material is intended for those coming to the subject for the first time and will provide a secure foundation from which to move into non-linear flight dynamics, simulation and advanced flight control. Placing emphasis on dynamics and their importance to flying and handling qualities it is accessible to both the aeronautical engineer and the control engineer. Emphasis on the design of flight control systems Intended for undergraduate and postgraduate students studying aeronautical subjects and avionics, systems engineering, control engineering Provides basic skills to analyse and evaluate aircraft flying qualities
Author: Charles E. Dole
Publisher: John Wiley & Sons
ISBN: 9780471370062
Category : Science
Languages : en
Pages : 332
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Book Description
The classic text for pilots on flight theory and aerodynamics?now in an updated Second Edition Flight Theory and Aerodynamics, the basic aeronautics text used by the United States Air Force in their Flying Safety Officer course, is the book that brings the science of flight into the cockpit. Designed for the student with little engineering or mathematical background, the book outlines the basic principles of aerodynamics and physics, using only a minimal amount of high school?level algebra and trigonometry necessary to illustrate key concepts. This expanded seventeen chapter Second Edition reflects the cutting edge of aeronautic theory and practice, and has been revised, reorganized, and updated with 30% new information?including a new chapter on helicopter flight. Central to the book?s structure is a clear description of aeronautic basics?what lifts and drives an aircraft, and what forces work for and against it?all detailed in the context of the design and analysis of today?s aircraft systems: Atmosphere and airspeed measurement Airfoils and aerodynamic forces Lift and drag Jet aircraft basic and applied performance Prop aircraft basic and applied performance Slow and high-speed flight Takeoff, landing, and maneuvering performance The book?s practical, self-study format includes problems at the end of each chapter, with answers at the back of the book, as well as chapter-end summaries of symbols and equations. An ideal text for the USN Aviation Safety Officer and the USAAA?s Aviation Safety Officer courses, as well as for professional pilots, student pilots, and flying safety personnel, Flight Theory and Aerodynamics is a complete and accessible guide to the subject, updated for the new millennium.
Author: J. Gordon Leishman
Publisher: Cambridge University Press
ISBN: 9780521660600
Category : Technology & Engineering
Languages : en
Pages : 496
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Book Description
An internationally recognized expert explains the aerodynamic principles of helicopters and other rotating-wing vertical lift aircraft. Besides the history of helicopter flight, basic methods of analysis, and performance and design issues, Leishman covers airfoil flows, unsteady aerodynamics, dynamic stall, and rotor wakes. Each chapter includes homework problems.
Author: John David Anderson
Publisher: Cambridge University Press
ISBN: 9780521669559
Category : Science
Languages : en
Pages : 498
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Book Description
Authoritative, highly readable history of aerodynamics and the major theorists and their contributions.
