Libros de Ingeniería aeronáutica y astronáutica, página 2 de 53

Based on the author's best-selling text Aircraft Structures for Engineering Students, this brief book covers the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work set the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. Numerous worked examples, illustrations, and sample problems show how to apply the concepts to realistic situations. Self-contained, this value-priced book is an excellent resource for anyone learning the subject. Based on the author's best-selling text Aircraft Structures for Engineering Students, this Intro version covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aeroelasticity. It features systematic step by step procedures in the worked examples. It is self-contained, with complete derivations for key equations.

"Providing an early introduction to STEM education, this book uses simple text and labeled photographs to examine a wide range of exciting machines used at the airport, revealing how each machine solves a particular problem. Machines covered include jet airplanes, staircases on wheels, scanners, conveyor belts, radars, and more!"

Master's Thesis from the year 2008 in the subject Engineering - Aerospace Technology, grade: A, University of Southampton, course: Computational Aerodynamics, language: English, abstract: Wing-in-ground effect (WIG) vehicles offer an exciting capability to fill the enormous void between speed of an aircraft and the payload capacity of a ship. WIG vehicles would be able to move cargo and passengers faster than a ship and more economical than an aircraft. Ground effect is a phenomenon that occurs on all wings flying close to the ground or a surface. The aim of this project is to investigate the behavior of wings (NACA/DHMTU series) in ground effect (on a fixed/variable terrain) using Fluent CFD package. The NACA 0012 and DHMTU series used in this project are designed specifically to fly in close proximity to the ground. The performance of the NACA/ DHMTU airfoils is examined for the lift and the drag coefficients at different altitudes with varying angle of attack. The results are compared to experimental data that is available to assess the accuracy of the CFD simulation.

Incredible high tech spacecraft allow us to explore the depths of outer space. How are these amazing machines built? Get ready to find out!

Presents a Compound Control Methodology for Flight VehiclesIncludes overview chapters to flight control, sliding mode control (SMC), active disturbance rejection control (ADRC) and compound controlWritten by leading experts in the fieldCompound Control Methodology for Flight Vehicles focuses on new control methods for flight vehicles. In this monograph the concept of compound control is introduced. It is demonstrated that both Sliding Mode Control (SMC) and Active Disturbance Rejection Control (ADRC) have their own advantages and limitations, i.e., chattering of SMC and the observability of extended state observer (ESO), respectively. It is shown that compound control combines their advantages and improves the performance of the closed-loop systems. The book is self-contained, providing sufficient mathematical foundations for understanding the contents of each chapter. It will be of significant interest to scientists and engineers engaged in the field of flight vehicle control.

Proven techniques for deriving the basic aerodynamic properties of axisymmetric-shaped bodies with the minimum amount of time and effort Aerodynamics of Missiles and Rockets describes the basic aerodynamics model used in the widespread Analytical Initial Missile Synthesis (AIMS) computer code for symmetric missile and rocket sizing and design. It is a collection of empirical, semi-empirical and theoretical aerodynamics engineering methods for a component build-up approach to aerodynamics prediction. This book serves as an on-the-job application manual and desk reference for the prediction of basic aerodynamics. It can also be used for courses in applied aerodynamics in Mechanical and Aerospace Engineering programs and for short courses in industry and government. This practical guide provides an alternative approach to utilizing numerous, complex, stand-alone computer codes, but is also a good complement to these codes. The book offers insight into the methods and techniques used to derive answers and correct magnitudes generated by code, giving confidence in final results. Features a Microsoft Excel file that automates calculations and provides complete tabulated output for missile and rocket geometry and design, and design and for rapid assessments of aerodynamic properties based on changes in geometry or flight conditions On-the-job application manual and desk reference for the prediction of basic aerodynamics Combination of long-standing, empirical and semi-empirical techniques with classical aerodynamic theory A component build-up approach utilized, with body and wing/tail surface aerodynamics determined separately and then combined for total configuration zero-lift drag, lift, center of pressure location, and pitching moment

The International Conference on Intelligent Unmanned Systems 2011 was organized by the International Society of Intelligent Unmanned Systems and locally by the Center for Bio-Micro Robotics Research at Chiba University, Japan. The event was the 7th conference continuing from previous conferences held in Seoul, Korea (2005, 2006), Bali, Indonesia (2007), Nanjing, China (2008), Jeju, Korea (2009), and Bali, Indonesia (2010). ICIUS 2011 focused on both theory and application, primarily covering the topics of robotics, autonomous vehicles, intelligent unmanned technologies, and biomimetics. We invited seven keynote speakers who dealt with related state-of-the-art technologies including unmanned aerial vehicles (UAVs) and micro air vehicles (MAVs), flapping wings (FWs), unmanned ground vehicles (UGVs), underwater vehicles (UVs), bio-inspired robotics, advanced control, and intelligent systems, among others. This book is a collection of excellent papers that were updated after presentation at ICIUS2011. All papers that form the chapters of this book were reviewed and revised from the perspective of advanced relevant technologies in the field. The aim of this book is to stimulate interactions among researchers active in the areas pertinent to intelligent unmanned systems.

This book provides a comprehensive guide to the derivation of computational models from basic physical & mathematical principles, giving the reader sufficient information to be able to represent the basic architecture of air vehicles and their embedded systems. Highly relevant to practitioners, it takes into account the multi-disciplinary nature of aerospace products and the integrated nature of the models needed to represent them. Following on from Volume 1- Platform Kinematics and Synthetic Environment -- which focuses on the modelling of the environment in which aircraft operate -- this book focuses on the modelling of the aerospace vehicles (aircraft and rotorcraft) themselves. Computational Modelling and Simulation of Aircraft and the Environment represents a development of the existing Aerospace series titles from Moir and Seabridge, as the author draws on some of the same examples used in previous works and dissects them mathematically -- thus giving a degree of commonality with earlier books in the series. More high level, detailed mathematics will be allocated to the appendices in order to render the main body of the material digestible as an introductory level text. Includes chapters on dynamics and control, flight dynamics & physics, generic aircraft and rotorcraft, vehicle and mission systems, and integration, operability & interoperability Serves as both a student text and practitioner reference Follows on from previous Aerospace series titles, taking some of the same examples used in these texts and dissecting them mathematically Accompanied by a website at www.wiley.com/go/diston which houses software, animations and useful weblinks.

The Aircraft Designers: A Grumman Historical Perspective tells the behind-the-scenes story of the designers and engineers who conceived and built Grumman aircraft from the founding of the company in 1929 until its 1994 acquisition by Northrop. While Grumman aircraft have been previously documented, The Aircraft Designers focuses instead on the people, disciplines, processes, and anecdotes behind the creation of such past icons as the F6F Wildcat and TBF Avenger and modern-day weapon systems like the F-14 Tomcat, E-2 Hawkeye, EA-6B Prowler, and Joint STARS. Michael Ciminera has identified key team members who contributed to the creation and development of each new design, creating an unparalleled historical record of the aeronautical achievements of the Grumman Corporation. He has also chronicled the evolution from the aircraft design of the past, which bore the earmark of the chief engineer/designer, to today's complex aircraft systems, which require a significant team effort involving such disciplines as aerodynamics, structures, propulsion, avionics, systems analysis, software, simulation, testing, and much more. The Aircraft Designers provides a unique insight into the leadership traits, technical skills, and lasting contributions of Grumman's designers. It will stand as the definitive historical account of the people who made Grumman aircraft a reality.

Global Aeronautical Communication, Navigation, and Surveillance (CNS): Volume 1 - Theory introduces the basic theoretical principles of communications, space technology, and antenna technology and their use in air traffic control (ATC) and air traffic management (ATM) systems. Topics Discussed * Development of airborne radio and satellite CNS and how they improve determination, safety, security, and distress alerting as well as enabling more cost-effective flight and ground infrastructures * Fundamentals of space platforms and orbital parameters, laws of satellite motion, new types of launching systems, satellite orbits and geometric relations, spacecraft configuration, payload structure, and satellite link design * Transmission systems, including discussion of modulation, demodulation, coding, error correction, multiple access, and mobile Internet * Airborne antenna systems * Propagation effects important for aeronautical requirements Special Features * A look into the past, present, and future of radio and satellite technologies * Theoretical guidelines, ready-to-use references, and performance evaluations

Civil Avionics Systems, Second Edition is an updated and in-depth practical guide to integrated avionic systems as applied to civil aircraft. This new edition has been expanded to include the latest developments in modern avionics. It describes avionic systems and potential developments in the field to help educate students and practitioners in the process of designing, building, and operating modern aircraft in the contemporary aviation system. Integration is a predominant theme of the book, since even as aircraft systems are becoming more integrated and complex, so are the economic, political, and technical environments in which they operate. Key features: content that is based on many years of practical industrial experience by the authors on a range of civil and military projects; focus on the integration and interconnectedness of systems in modern complex aircraft; updated contents in light of latest applications; and, substantial new material on avionics technology, software, and system safety. The authors are all recognized experts, and between them have over 140 years of experience in the aircraft industry. Their direct and accessible style ensures that Civil Avionics Systems, Second Edition is a must-have guide to integrated avionic systems in modern aircraft for aerospace students and practitioners.

La preparación de este libro ha estado guiada por la idea de que sirva como material básico para la docencia de esta disciplina en los grados de ingeniería de los nuevos planes de estudios. El libro

Modern aircraft manufacturing involves drilling and countersinking hundreds of thousands to millions of holes. Doing this work by hand accounts for 65% of the cost of airframe assembly, 85% of the quality issues, and 80% of the lost time due to injuries. Automated drilling and countersinking replaces traditional hand methods and involves using numeric control machinery to drill and countersink a finished hole one shot (drilling a finished hole without using pilot holes or tool changes). This is a proven cost reducing technology that improves quality where it has been applied successfully. The focus of this book is on automating the process of drilling and countersinking holes during airframe manufacturing. Since this is the area of greatest return on investment for airframe producers, the book provides a stepped approach for evaluating possible areas for applying automation and a detailed description of the process for choosing, acquiring, and transitioning the right machinery for success. It also provides a vision for a 10- to 15-year future state of airframe manufacture. Readers will use the information to: Understand the evolution of automated/mechanized drilling and countersinking airframes. Access decision models and matrices to help evaluate the feasibility of applying automation/mechanization to any airframe. Gain access to a step-by-step procedure to select the right piece of machinery. Learn the necessary processes for testing and transitioning machinery to production. Assess and acquire data to evaluate the effect of the process. Choose and train the right individuals to manage and run the machinery. Conduct cost benefit analysis models. Make recommendations for maintenance and spares. Address socio-economic factors to reconfigure a facility from hand to automated activities. No other book provides such detailed technical, economic, and social information about automating the single largest contributor to airframe cost.

This volume contains an investigation of remotely piloted research vehicle (RPRV) and unmanned aircraft system (UAS) mishaps and will examine their causes, consequences, resultant corrective actions, and lessons learned. Most undesired outcomes usually do not occur because of a single event, but rather from a series of events and actions involving equipment malfunctions and/or human factors. This book comprises a series of case studies focusing mostly on accidents and incidents involving experimental aircraft. The information provided should be of use to flight-test organizations, aircraft operators, educators, and students, among others. These lessons are not unique to the UAS environment and are also applicable to human aviation and space flight activities. Common elements include crew resource management, training, mission planning issues, management and programmatic pressures (e.g., schedule, budget, resources), cockpit/control station design, and other factors. (Contains copyright material)

The Electronic Navigation Research Institute (ENRI) held its third International Workshop on ATM / CNS in 2013 with the theme of "Drafting the future sky". There is worldwide activity taking place in the research and development of modern air traffic management (ATM) and its enabling technologies in Communication, Navigation and Surveillance (CNS). Pioneering work is necessary to contribute to the global harmonization of air traffic management and control. At this workshop, leading experts in research, industry and academia from around the world met to share their ideas and approaches on ATM/CNS related topics.

Alta tecnología y movilidad. Desde los inicios hasta hoy.

Morphing Aerospace Vehicles and Structures provides a highly timely presentation of the state-of-the-art, future directions and technical requirements of morphing aircraft. Divided into three sections it addresses morphing aircraft, bio-inspiration, and smart structures with specific focus on the flight control, aerodynamics, bio-mechanics, materials, and structures of these vehicles as well as power requirements and the use of advanced piezo materials and smart actuators. The tutorial approach adopted by the contributors, including underlying concepts and mathematical formulations, unifies the methodologies and tools required to provide practicing engineers and applied researchers with the insight to synthesize morphing air vehicles and morphing structures, as well as offering direction for future research.

El objetivo de la aerodinámica civil es la estimación de las cargas aerodinámicas (fuerzas y momentos) que genera el flujo del aire alrededor de los cuerpos inmersos en la capa límite terrestre. Pa